OPS 9442 (DSCS 2-12) DEB, 59989
Orbit data source: Space-Track
OPS 9442 (DSCS 2-12) DEB, 59989 is space debris in GEO originally from a launch on Thu, 14 Dec 1978 UTC launched from the Air Force Eastern Test Range (AFETR). 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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59989 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 OPS 9442 (DSCS 2-12) DEB
1 59989U 78113E 26170.57329832 -.00000164 00000-0 00000-0 0 9997
2 59989 8.1666 302.3961 0171436 87.2722 274.7717 0.98457392 45240Epoch: 2026-06-19T13:45Z
TLE epoch observation values (Epoch: 2026-06-19T13:45:32.974Z)
Latitude
-0°
Longitude
-171.7129°
Altitude
36,257.054 km
Speed
3.059 km/s
True Right ascension
20h 09m 53s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
00:50:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,035.784 km
Perigee altitude
35,572.331 km
Semi-major axis
42,682.195 km
Eccentricity
0.01714
Inclination
8.1666°
RAAN
302.3961°
Arg. of periapsis
87.2722°
True anomaly
272.81088°
Mean anomaly
274.7717°
Eccentric anomaly
273.79159°
Mean motion
0.24613 °/min
Orbital period
1,462.61 mins
BSTAR
0
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Other satellites on launch #113 in the year 1978 (1978-12-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OPS 9442 (DSCS 2-12) DEB Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| OPS 9442 (DSCS 2-12) DEB is likely not visible in the next few days. |
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59989 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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