NIMBUS 2 DEB, 28620
Orbit data source: Space-Track
NIMBUS 2 DEB, 28620 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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28620 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | SSO |
| Last TLE update | 2 days 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 2 days ago
0 NIMBUS 2 DEB
1 28620U 66040AK 25070.16498400 .00002800 00000-0 44395-2 0 9997
2 28620 100.4363 313.9957 0043502 46.5259 104.8093 13.50156260989201Epoch: 2025-03-11T03:57Z
Definitive object data (Epoch: 2025-03-11T03:57:34.617Z)
| Latitude | 27.71834° |
| Longitude | -88.94538° |
| Altitude | 1,083.363 km |
| Speed | 7.309 km/s |
| True Right ascension | 09h 18m 04s |
| True Declination | 27° 34' 59" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 64.87308° |
| Longitude | -69.23132° |
| Altitude | 1,072.437 km |
| Speed | 7.327 km/s |
| Apparent Right ascension | 01h 30m 26s |
| Apparent Declination | 51° 51' 05" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:44:51 |
| Azimuth | 344.007° N |
| Elevation | 4.602° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,101.421 km |
| Perigee altitude | 1,036.627 km |
| Semi-major axis | 7,447.161 km |
| Eccentricity | 0.0043502 |
| Inclination | 100.4363° |
| RAAN | 313.9957° |
| Arg. of periapsis | 46.5259° |
| True anomaly | 105.29056° |
| Mean anomaly | 104.8093° |
| Eccentric anomaly | 105.05° |
| Mean motion | 3.3772 °/min |
| BSTAR | 0.0044395 |
| Orbital period | 106.6 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 | 2025-03-13 15:48:35.976Z | 152.337° SSE | 2025-03-13 15:52:35.976Z | 104.54° ESE | 43.39° | 2025-03-13 15:58:35.976Z | 348.855° N |
| 5 mins | 2025-03-13 17:36:35.976Z | 245.517° WSW | 2025-03-13 17:38:35.976Z | 267.162° W | 16.196° | 2025-03-13 17:41:35.976Z | 298.365° NW |
| 11 mins | 2025-03-14 04:44:35.976Z | 29.211° NE | 2025-03-14 04:49:35.976Z | 116.733° SE | 39.963° | 2025-03-14 04:55:35.976Z | 180.829° SSW |
| 8 mins | 2025-03-14 06:30:35.976Z | 338.261° N | 2025-03-14 06:33:35.976Z | 302.571° NW | 23.222° | 2025-03-14 06:38:35.976Z | 249.459° W |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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