NIMBUS 2 DEB, 28978
Orbit data source: Space-Track
NIMBUS 2 DEB, 28978 is space debris in SSO originally from a launch on Sun, 15 May 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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28978 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | SSO |
| Last TLE update | 19 hours ago |
| Origin | |
| Manufacturer | Unknown |
| Mission | Spacecraft |
| Bus & Motor | Unknown |
| Mass | Unknown |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 19 hours ago
0 NIMBUS 2 DEB
1 28978U 66040AP 25069.68567102 .00002694 00000-0 42496-2 0 9995
2 28978 100.3802 339.6587 0044583 67.4349 311.3132 13.50503953867311Epoch: 2025-03-10T16:27Z
Definitive object data (Epoch: 2025-03-10T16:27:21.976Z)
| Latitude | 18.04615° |
| Longitude | -79.18613° |
| Altitude | 1,050.777 km |
| Speed | 7.339 km/s |
| True Right ascension | 22h 25m 01s |
| True Declination | 17° 56' 57" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -72.65099° |
| Longitude | 69.35318° |
| Altitude | 1,129.742 km |
| Speed | 7.271 km/s |
| Apparent Right ascension | 05h 02m 36s |
| Apparent Declination | -61° 36' 05" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 15:41:30 |
| Azimuth | 202.993° SW |
| Elevation | -65.042° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,100.938 km |
| Perigee altitude | 1,034.546 km |
| Semi-major axis | 7,445.879 km |
| Eccentricity | 0.0044583 |
| Inclination | 100.3802° |
| RAAN | 339.6587° |
| Arg. of periapsis | 67.4349° |
| True anomaly | 310.92806° |
| Mean anomaly | 311.3132° |
| Eccentric anomaly | 311.12077° |
| Mean motion | 3.37807 °/min |
| BSTAR | 0.0042496 |
| Orbital period | 106.57 mins |
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Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)
NIMBUS 2 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-03-11 17:23:27.740Z | 144.556° SSE | 2025-03-11 17:27:27.740Z | 87.922° E | 41.326° | 2025-03-11 17:33:27.740Z | 352.186° N |
| 7 mins | 2025-03-11 19:10:27.740Z | 234.008° WSW | 2025-03-11 19:13:27.740Z | 268.432° W | 19.249° | 2025-03-11 19:17:27.740Z | 309.762° NW |
| 10 mins | 2025-03-12 06:19:27.740Z | 35.155° NE | 2025-03-12 06:23:27.740Z | 93.931° ESE | 36.731° | 2025-03-12 06:29:27.740Z | 173.179° S |
| 9 mins | 2025-03-12 08:04:27.740Z | 346.145° N | 2025-03-12 08:08:27.740Z | 297.39° NW | 26.002° | 2025-03-12 08:13:27.740Z | 242.981° WSW |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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