DMSP 5D-2 F6 DEB, 40914
Orbit data source: Space-Track
DMSP 5D-2 F6 DEB, 40914 is space debris in SSO originally from a launch on Tue, 21 Dec 1982 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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40914 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 DMSP 5D-2 F6 DEB
1 40914U 82118G 24282.37058455 .00074353 00000-0 14149-1 0 9995
2 40914 98.4292 132.6962 0014371 28.3007 331.8972 14.63597326444381
Epoch: 2024-10-08T08:53Z
TLE epoch observation values (Epoch: 2024-10-08T08:53:38.505Z)
Latitude
-0.00002°
Longitude
-18.19904°
Altitude
675.617 km
Speed
7.524 km/s
True Right ascension
08h 50m 47s
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
13:16:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
688.811 km
Perigee altitude
668.528 km
Semi-major axis
7,056.806 km
Eccentricity
0.00144
Inclination
98.4292°
RAAN
132.6962°
Arg. of periapsis
28.3007°
True anomaly
331.8195°
Mean anomaly
331.8972°
Eccentric anomaly
331.85836°
Mean motion
3.66126 °/min
Orbital period
98.33 mins
BSTAR
0.014149
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Other satellites on launch #118 in the year 1982 (1982-12-21 UTC)
DMSP 5D-2 F6 DEB Visibility forecast
Observer location: undefined°, undefined°
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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4 mins | 2025-08-27 04:28:43.313Z | 35.347° NE | 2025-08-27 04:30:43.313Z | 120.953° SE | 32.901° | 2025-08-27 04:32:43.313Z | 172.599° S |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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