Gemini VII Orbital Cylindrical Object & Thruster Plume Correlation
Low Earth Orbit over Cape Canaveral / Western Atlantic Sector (28.5°, -80.6°) • Event Date: 1965-12-04 • NARA RG 255 / NASA Magazine 29-B Frames S65-63722 & S65-63723
During Revolution 3 of the Gemini VII mission on December 4, 1965, Command Pilot Frank Borman and Pilot Jim Lovell photographed a cylindrical metallic-albedo object accompanied by a luminous multi-lobed plume at 301 km (187 mi / 987,500 ft) altitude and 17,023 mph (7.61 km/s). PURSUE Release 01 provides 4K micro-densitometric scans of the original Hasselblad 70mm Orbital Film paired with NORAD Space Surveillance Radar two-line element (TLE) reconstructions. Observers tracking low-Earth orbital cylinders, upper-stage boosters, and bright LEO passes can resolve magnitude +2.5 to +6.0 targets using 15x70 astronomy binoculars[↗] or a plate-solved smart telescope[↗] with satellite ephemeris tracking.
Dual Imperial (ft, mi, mph) & Metric (m, km, km/s) Kinematic Table
Local Gemma Multi-Sensor & CNEOS Correlation Memo
Primary sensor modalities (Hasselblad 70mm Orbital Film, 35mm Photogrammetry, NORAD Space Surveillance Radar) recorded the 7.6 m / 25 ft target at 301 km / 187 mi (301,000 m / 987,500 ft) traveling at 17,023 mph / 7.61 km/s (Mach 22.2 Orbital) over signed coordinates (28.5°, -80.6°). Orbital tracking at 301,000 m (987,500 ft / 301 km / 187 mi) and 7.61 km/s (17,023 mph / Mach 22.2) places the object in co-elliptical Low Earth Orbit (28.87° inclination). The 7.6 m (25 ft) cylindrical body exhibits low relative angular rate against the Gemini VII spacecraft.
Nearest cataloged NASA JPL CNEOS bolide airburst is cneos-fb-26-202511111739 at a great-circle distance of 154.9 km / 96.3 mi (North American Continental Sector, 2025-11-11 17:39:51 UTC). Calculated CNEOS atmospheric bolide match probability is 53% versus a kinematic anomaly score of 57/100.
TLE Orbital Shell Assessment: NORAD 01804 • Titan II Upper Stage LEO Shell (28.52° inc, ~301 km) [J2-Propagated Sub-Point (-21.4°, -89.3°), Ground Δ=5626 km]. Satellite specular flare likelihood is evaluated at 61%. Observers tracking low-Earth orbital cylinders, upper-stage boosters, and bright LEO passes can resolve magnitude +2.5 to +6.0 targets using 15x70 astronomy binoculars[↗] or a plate-solved smart telescope[↗] with satellite ephemeris tracking.
Frequently Asked Questions — Multi-Sensor UAP & CNEOS Verification
What are the exact Imperial and Metric altitude, speed, and size measurements for Gemini VII Orbital Cylindrical Object & Thruster Plume Correlation?
Official RELEASE_01 telemetry places the 25 ft (7.6 m) object at an altitude of 301 km / 187 mi (301,000 m / 987,500 ft) and speed of 17,023 mph / 7.61 km/s (Mach 22.2 Orbital) over (28.5°, -80.6°).
Did NASA CNEOS fireball sensors or orbital TLE satellite shells match pursue-r1-gemini-vii-1965?
Spatiotemporal CNEOS + J2 TLE analysis for Gemini VII Orbital Cylindrical Object & Thruster Plume Correlation at (28.5°, -80.6°), altitude 301.00 km (187.03 mi / 987,533 ft), velocity 17,023 mph (7.61 km/s): Nearest cataloged NASA CNEOS bolide is cneos-fb-26-202511111739 at 154.9 km / 96.3 mi great-circle separation (2025-11-11 17:39:51, Δt=21893 days), yielding 53% bolide match probability, 61% J2-propagated TLE flare likelihood, and 57/100 kinematic anomaly score.
Which official war.gov/ufo, AARO, and NARA archives document case pursue-r1-gemini-vii-1965?
This case is published under PURSUE Release 01 — Historic Spaceflight & Orbital Anomaly Photography (Gemini VII & Apollo 17 Archive) (2026-05-08) via https://www.war.gov/ufo/, https://www.aaro.mil, and https://www.archives.gov/research/topics/uaps (NARA RG 255 / NASA Magazine 29-B Frames S65-63722 & S65-63723).
Gemini VII Orbital Cylindrical Object & Thruster Plume Correlation (RELEASE_01) (H = 8.4, Vmag ≈ -3.8) reaches high surface brightness suitable for 70mm large-aperture binoculars[↗].
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