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: 1 day ago

TLE from 1 day ago
0 OV1-9 R/B
1 02622U 66111D   25256.09209612  .00000697  00000-0  27419-3 0  9994
2 02622  99.0983 293.7551 2224976 131.6135 249.8153 10.49295917215823
Epoch: 2025-09-13T02:12Z
TLE epoch observation values (Epoch: 2025-09-13T02:12:37.104Z)
Latitude
0.00003°
Longitude
-91.72993°
Altitude
3,450.853 km
Speed
5.992 km/s
True Right ascension
19h 35m 01s
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
20:02:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,393.009 km
Perigee altitude
472.258 km
Semi-major axis
8,810.771 km
Eccentricity
0.2225
Inclination
99.0983°
RAAN
293.7551°
Arg. of periapsis
131.6135°
True anomaly
228.48189°
Mean anomaly
249.8153°
Eccentric anomaly
238.89951°
Mean motion
2.62435 °/min
Orbital period
137.18 mins
BSTAR
0.00027419
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Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)

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