OV1-20/OV1-21 DEB, 5384

Orbit data source: Space-Track

OV1-20/OV1-21 DEB, 5384 is space debris in LEO originally from a launch on Sat, 07 Aug 1971 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
5384, 1971-067N
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GOYR?
Mission
Spacecraft
Bus & Motor
AVL-802 CANISTER, Unknown motor
Mass
~12 kg wet, ~12 kg dry
Launch date (UTC)
1971-08-07 (55 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 OV1-20/OV1-21 DEB
1  5384U 71067N   26099.12724318  .00000305  00000-0  11905-3 0  9992
2  5384  87.6259  52.4827 0076891 301.6553  57.7154 14.25269800833393
Epoch: 2026-04-09T03:03Z
TLE epoch observation values (Epoch: 2026-04-09T03:03:13.810Z)
Latitude
-0.00008°
Longitude
169.29544°
Altitude
781.426 km
Speed
7.478 km/s
True Right ascension
03h 29m 55s
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
14:55:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
859.77 km
Perigee altitude
749.314 km
Semi-major axis
7,182.679 km
Eccentricity
0.00769
Inclination
87.6259°
RAAN
52.4827°
Arg. of periapsis
301.6553°
True anomaly
58.46411°
Mean anomaly
57.7154°
Eccentric anomaly
58.08937°
Mean motion
3.56544 °/min
Orbital period
100.97 mins
BSTAR
0.00011905
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