OV1-5 DEB, 5599

Orbit data source: Space-Track

OV1-5 DEB, 5599 is 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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Identifier
5599, 1966-025G
Orbit
LEO
Country
Flag of USUS
Related business
Flag of USAir Force Systems Command (OAR legacy assets) (US)
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1966-03-30 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 OV1-5 DEB
1 05599U 66025G   25294.57953798  .00054167  00000-0  66640-2 0  9999
2 05599 144.6131 202.0028 0019590  44.6238 315.6046 14.81292114 68951
Epoch: 2025-10-21T13:54Z
TLE epoch observation values (Epoch: 2025-10-21T13:54:32.081Z)
Latitude
-0.00003°
Longitude
-36.8963°
Altitude
614.428 km
Speed
7.559 km/s
True Right ascension
13h 28m 00s
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
17:30:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.105 km
Perigee altitude
614.653 km
Semi-major axis
7,006.516 km
Eccentricity
0.00196
Inclination
144.6131°
RAAN
202.0028°
Arg. of periapsis
44.6238°
True anomaly
315.44727°
Mean anomaly
315.6046°
Eccentric anomaly
315.52596°
Mean motion
3.70075 °/min
Orbital period
97.28 mins
BSTAR
0.006664
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