OV1-9 R/B, 2622

Orbit data source: Space-Track

OV1-9 R/B, 2622 is space debris in LEO originally from a launch on Sun, 11 Dec 1966 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
2622, 1966-111D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
125 kg wet, 125 kg dry
Launch date (UTC)
1966-12-11 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.1 m
Radar Cross Section
1.347 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 OV1-9 R/B
1 02622U 66111D   25260.95496213  .00000966  00000-0  37820-3 0  9995
2 02622  99.0974 296.4864 2224792 124.0531 259.2041 10.49305577216334
Epoch: 2025-09-17T22:55Z
TLE epoch observation values (Epoch: 2025-09-17T22:55:08.728Z)
Latitude
-0.00001°
Longitude
-44.42346°
Altitude
3,190.317 km
Speed
6.173 km/s
True Right ascension
19h 45m 56s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:39:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,392.781 km
Perigee altitude
472.378 km
Semi-major axis
8,810.716 km
Eccentricity
0.22248
Inclination
99.0974°
RAAN
296.4864°
Arg. of periapsis
124.0531°
True anomaly
236.04417°
Mean anomaly
259.2041°
Eccentric anomaly
247.43301°
Mean motion
2.62438 °/min
Orbital period
137.18 mins
BSTAR
0.0003782
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Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)

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