OPS 4682 DEB, 38426

Orbit data source: Space-Track

OPS 4682 DEB, 38426 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
38426, 1965-027EF
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: 19 hours ago

TLE from 19 hours ago
0 OPS 4682 DEB
1 38426U 65027EF  26150.37157287  .00000736  00000-0  25515-2 0  9993
2 38426  90.2440   9.6714 0034212 193.7797 166.2393 12.96126414632755
Epoch: 2026-05-30T08:55Z
TLE epoch observation values (Epoch: 2026-05-30T08:55:03.895Z)
Latitude
0.00002°
Longitude
-11.98339°
Altitude
1,305.628 km
Speed
7.192 km/s
True Right ascension
00h 38m 41s
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
13:40:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,300.615 km
Perigee altitude
1,248.253 km
Semi-major axis
7,652.571 km
Eccentricity
0.00342
Inclination
90.244°
RAAN
9.6714°
Arg. of periapsis
193.7797°
True anomaly
166.33217°
Mean anomaly
166.2393°
Eccentric anomaly
166.28577°
Mean motion
3.24214 °/min
Orbital period
111.04 mins
BSTAR
0.0025515
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