OPS 4682 DEB, 38458

Orbit data source: Space-Track

OPS 4682 DEB, 38458 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
38458, 1965-027FP
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
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 OPS 4682 DEB
1 38458U 65027FP  26116.44508852  .00000272  00000-0  96382-3 0  9992
2 38458  90.2473   5.6839 0031713  55.2678 305.1420 12.93400365606970
Epoch: 2026-04-26T10:40Z
TLE epoch observation values (Epoch: 2026-04-26T10:40:55.648Z)
Latitude
0.00002°
Longitude
-8.99697°
Altitude
1,276.983 km
Speed
7.224 km/s
True Right ascension
00h 22m 44s
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
05:43:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,309.494 km
Perigee altitude
1,260.888 km
Semi-major axis
7,663.328 km
Eccentricity
0.00317
Inclination
90.2473°
RAAN
5.6839°
Arg. of periapsis
55.2678°
True anomaly
304.84416°
Mean anomaly
305.142°
Eccentric anomaly
304.99315°
Mean motion
3.23532 °/min
Orbital period
111.27 mins
BSTAR
0.00096382
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