OV1-5 DEB, 27880 (Decayed)
Orbit data source: Space-Track
OV1-5 DEB, 27880 was space debris in LEO originally from a launch on Wed, 30 Mar 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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27880 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
3 months ago
Origin
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & history
TLE from 3 months ago
0 OV1-5 DEB
1 27880U 66025H 25104.32435417 .02799559 00000-0 25165-1 0 9991
2 27880 144.6136 12.8047 0019148 194.0677 165.9522 15.63724237580194Epoch: 2025-04-14T07:47Z
TLE epoch observation values (Epoch: 2025-04-14T07:47:04.2Z)
Latitude
-0.00003°
Longitude
53.29629°
Altitude
388.385 km
Speed
7.672 km/s
True Right ascension
00h 51m 13s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
Orbital elements
Apogee altitude
393.097 km
Perigee altitude
367.215 km
Semi-major axis
6,758.293 km
Eccentricity
0.00191
Inclination
144.6136°
RAAN
12.8047°
Arg. of periapsis
194.0677°
True anomaly
166.00534°
Mean anomaly
165.9522°
Eccentric anomaly
165.97878°
Mean motion
3.9065 °/min
Orbital period
92.15 mins
BSTAR
0.025165
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Other satellites on launch #25 in the year 1966 (1966-03-30 UTC)
OV1-5 DEB Visibility
Observer location: undefined°, undefined°
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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