OPS 4682 DEB, 29060

Orbit data source: Space-Track

OPS 4682 DEB, 29060 is space debris in LEO originally from a launch on Sat, 03 Apr 1965 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
29060, 1965-027BK
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-04-03 (61 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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 OPS 4682 DEB
1 29060U 65027BK  26175.29601689 -.00000029  00000-0 -12898-3 0  9993
2 29060  90.2417  10.3994 0030612 182.6564 359.7265 12.94827667465039
Epoch: 2026-06-24T07:06Z
TLE epoch observation values (Epoch: 2026-06-24T07:06:15.859Z)
Latitude
-2.50762°
Longitude
171.36752°
Altitude
1,262.202 km
Speed
7.235 km/s
True Right ascension
12h 41m 33s
True Declination
-2° 29' 37"
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
10:36:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,302.996 km
Perigee altitude
1,256.112 km
Semi-major axis
7,657.691 km
Eccentricity
0.00306
Inclination
90.2417°
RAAN
10.3994°
Arg. of periapsis
182.6564°
True anomaly
359.72482°
Mean anomaly
359.7265°
Eccentric anomaly
359.72566°
Mean motion
3.23889 °/min
Orbital period
111.15 mins
BSTAR
-0.00012898
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