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: 11 hours ago

TLE from 11 hours ago
0 OV1-10 R/B
1 02621U 66111C   26081.24524578  .00000777  00000-0  88436-4 0  9994
2 02621  93.3993 168.0468 0056957  22.6216 337.7500 14.85470914161458
Epoch: 2026-03-22T05:53Z
TLE epoch observation values (Epoch: 2026-03-22T05:53:09.235Z)
Latitude
0.00002°
Longitude
-99.99605°
Altitude
578.409 km
Speed
7.591 km/s
True Right ascension
11h 12m 11s
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
21:31:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
648.793 km
Perigee altitude
569.2 km
Semi-major axis
6,987.133 km
Eccentricity
0.0057
Inclination
93.3993°
RAAN
168.0468°
Arg. of periapsis
22.6216°
True anomaly
337.50123°
Mean anomaly
337.75°
Eccentric anomaly
337.62578°
Mean motion
3.71616 °/min
Orbital period
96.87 mins
BSTAR
0.000088436
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Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)

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