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: 3 days ago

TLE from 3 days ago
0 OPS 4682 DEB
1 29060U 65027BK  26233.16128565  .00000301  00000-0  10475-2 0  9990
2 29060  90.2480  11.6807 0031106  37.4894  86.6135 12.94842104472525
Epoch: 2026-08-21T03:52Z
TLE epoch observation values (Epoch: 2026-08-21T03:52:15.080Z)
Latitude
55.63133°
Longitude
164.48866°
Altitude
1,290.329 km
Speed
7.217 km/s
True Right ascension
12h 48m 09s
True Declination
55° 28' 55"
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
14:03:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,303.317 km
Perigee altitude
1,255.677 km
Semi-major axis
7,657.634 km
Eccentricity
0.00311
Inclination
90.248°
RAAN
11.6807°
Arg. of periapsis
37.4894°
True anomaly
86.96941°
Mean anomaly
86.6135°
Eccentric anomaly
86.79144°
Mean motion
3.23893 °/min
Orbital period
111.15 mins
BSTAR
0.0010475
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