OPS 0856 DEB, 24647

Orbit data source: Space-Track

OPS 0856 DEB, 24647 is space debris in LEO originally from a launch on Fri, 19 Aug 1966 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
24647, 1966-077P
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1966-08-19 (60 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: 1 day ago

TLE from 1 day ago
0 OPS 0856 DEB
1 24647U 66077P   26118.80004736  .00029411  00000-0  26803+0 0  9990
2 24647  87.6350  59.9232 2199644  84.8127 321.5491  9.42287506564024
Epoch: 2026-04-28T19:12Z
TLE epoch observation values (Epoch: 2026-04-28T19:12:04.091Z)
Latitude
26.84715°
Longitude
-83.67201°
Altitude
1,693.477 km
Speed
7.533 km/s
True Right ascension
04h 04m 27s
True Declination
26° 43' 30"
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
07:46:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,170.019 km
Perigee altitude
1,005.663 km
Semi-major axis
9,465.978 km
Eccentricity
0.21996
Inclination
87.635°
RAAN
59.9232°
Arg. of periapsis
84.8127°
True anomaly
302.02778°
Mean anomaly
321.5491°
Eccentric anomaly
312.21492°
Mean motion
2.35665 °/min
Orbital period
152.76 mins
BSTAR
0.26803
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