OPS 4682 DEB, 19954

Orbit data source: Space-Track

OPS 4682 DEB, 19954 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
19954, 1965-027AZ
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-04-03 (62 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.070 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 OPS 4682 DEB
1 19954U 65027AZ  26288.42056926  .00000906  00000-0  27620-2 0  9992
2 19954  90.3878  83.2765 0031248 183.1450 205.0508 13.05319779791233
Epoch: 2026-10-15T10:05Z
TLE epoch observation values (Epoch: 2026-10-15T10:05:37.184Z)
Latitude
28.08239°
Longitude
-92.2905°
Altitude
1,266.365 km
Speed
7.214 km/s
True Right ascension
05h 32m 16s
True Declination
27° 56' 57"
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
15:22:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,262.234 km
Perigee altitude
1,214.633 km
Semi-major axis
7,616.571 km
Eccentricity
0.00312
Inclination
90.3878°
RAAN
83.2765°
Arg. of periapsis
183.145°
True anomaly
204.89972°
Mean anomaly
205.0508°
Eccentric anomaly
204.97521°
Mean motion
3.26516 °/min
Orbital period
110.26 mins
BSTAR
0.002762
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