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: 14 hours ago

TLE from 14 hours ago
0 OV1-20/OV1-21 DEB
1 05384U 71067N   26154.16914138  .00000297  00000-0  11453-3 0  9997
2 05384  87.6281  37.5490 0080672 120.8309 240.0853 14.25292526841236
Epoch: 2026-06-03T04:03Z
TLE epoch observation values (Epoch: 2026-06-03T04:03:33.815Z)
Latitude
-0.00004°
Longitude
85.02648°
Altitude
839.827 km
Speed
7.418 km/s
True Right ascension
02h 30m 11s
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
03:47:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
862.409 km
Perigee altitude
746.522 km
Semi-major axis
7,182.603 km
Eccentricity
0.00807
Inclination
87.6281°
RAAN
37.549°
Arg. of periapsis
120.8309°
True anomaly
239.28807°
Mean anomaly
240.0853°
Eccentric anomaly
239.68628°
Mean motion
3.5655 °/min
Orbital period
100.97 mins
BSTAR
0.00011453
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