OV1-10 R/B, 2621

Orbit data source: Space-Track

OV1-10 R/B, 2621 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
2621, 1966-111C
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
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 OV1-10 R/B
1 02621U 66111C   25338.92527477  .00001814  00000-0  20636-3 0  9994
2 02621  93.3987 122.0922 0058053  42.6426 317.9282 14.85182340145520
Epoch: 2025-12-04T22:12Z
TLE epoch observation values (Epoch: 2025-12-04T22:12:23.740Z)
Latitude
-0.00007°
Longitude
75.01856°
Altitude
586.112 km
Speed
7.583 km/s
True Right ascension
08h 08m 22s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
00:34:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.47 km
Perigee altitude
569.335 km
Semi-major axis
6,988.039 km
Eccentricity
0.00581
Inclination
93.3987°
RAAN
122.0922°
Arg. of periapsis
42.6426°
True anomaly
317.48004°
Mean anomaly
317.9282°
Eccentric anomaly
317.70436°
Mean motion
3.71544 °/min
Orbital period
96.89 mins
BSTAR
0.00020636
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Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)

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