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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5384 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
GOYR?
Mission
Spacecraft
Bus & Motor
AVL-802 CANISTER, Unknown motor
Mass
~12 kg wet, ~12 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OV1-20/OV1-21 DEB
1 05384U 71067N 25348.77438498 .00000342 00000-0 13430-3 0 9996
2 05384 87.6257 83.8574 0077294 316.7778 42.7364 14.25187377816961Epoch: 2025-12-14T18:35Z
TLE epoch observation values (Epoch: 2025-12-14T18:35:06.862Z)
Latitude
0.00001°
Longitude
81.39633°
Altitude
770.31 km
Speed
7.49 km/s
True Right ascension
05h 35m 25s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:18:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
860.339 km
Perigee altitude
749.299 km
Semi-major axis
7,182.956 km
Eccentricity
0.00773
Inclination
87.6257°
RAAN
83.8574°
Arg. of periapsis
316.7778°
True anomaly
43.34176°
Mean anomaly
42.7364°
Eccentric anomaly
43.03865°
Mean motion
3.56524 °/min
Orbital period
100.98 mins
BSTAR
0.0001343
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Other satellites on launch #67 in the year 1971 (1971-08-07 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OV1-20/OV1-21 DEB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-15 18:45:51.125Z | 358.224° N | 2025-12-15 18:49:51.125Z | 333.35° NNW | 44.804° | 2025-12-15 18:54:51.125Z | 182.238° SSW |
| 7 mins | 2025-12-16 06:06:51.125Z | 126.268° SE | 2025-12-16 06:09:51.125Z | 76.457° E | 25.985° | 2025-12-16 06:13:51.125Z | 24.872° NE |
| 7 mins | 2025-12-16 07:47:51.125Z | 230.33° WSW | 2025-12-16 07:50:51.125Z | 281.629° WNW | 27.349° | 2025-12-16 07:54:51.125Z | 336.792° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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