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
Cyl, 1.1 m
Radar Cross Section
1.347 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 OV1-10 R/B
1 02621U 66111C   25256.24631918  .00000586  00000-0  67973-4 0  9995
2 02621  93.3964  86.7483 0055780 336.2390  23.6259 14.84906061133254
Epoch: 2025-09-13T05:54Z
TLE epoch observation values (Epoch: 2025-09-13T05:54:41.977Z)
Latitude
-0.00004°
Longitude
5.59097°
Altitude
581.301 km
Speed
7.589 km/s
True Right ascension
05h 46m 59s
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
20:03:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
649.754 km
Perigee altitude
571.786 km
Semi-major axis
6,988.907 km
Eccentricity
0.00558
Inclination
93.3964°
RAAN
86.7483°
Arg. of periapsis
336.239°
True anomaly
23.88371°
Mean anomaly
23.6259°
Eccentric anomaly
23.75464°
Mean motion
3.71475 °/min
Orbital period
96.91 mins
BSTAR
0.000067973
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Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)

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