NIMBUS 2 DEB, 28612
Orbit data source: Space-Track
NIMBUS 2 DEB, 28612 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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28612 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 NIMBUS 2 DEB
1 28612U 66040AB 25287.87749678 .00003555 00000-0 36757-2 0 9993
2 28612 100.3773 145.7595 0045480 307.4432 69.1442 13.76171676666551Epoch: 2025-10-14T21:03Z
TLE epoch observation values (Epoch: 2025-10-14T21:03:35.721Z)
Latitude
16.77473°
Longitude
163.05317°
Altitude
967.89 km
Speed
7.375 km/s
True Right ascension
09h 30m 26s
True Declination
16° 40' 58"
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
17:59:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,008.241 km
Perigee altitude
941.358 km
Semi-major axis
7,352.937 km
Eccentricity
0.00455
Inclination
100.3773°
RAAN
145.7595°
Arg. of periapsis
307.4432°
True anomaly
69.6322°
Mean anomaly
69.1442°
Eccentric anomaly
69.3881°
Mean motion
3.44233 °/min
Orbital period
104.58 mins
BSTAR
0.0036757
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Other satellites on launch #40 in the year 1966 (1966-05-15 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.NIMBUS 2 DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-10-19 02:46:26.459Z | 34.238° NE | 2025-10-19 02:52:26.459Z | 106.104° ESE | 29.244° | 2025-10-19 02:57:26.459Z | 161.322° S |
| 10 mins | 2025-10-19 04:30:26.459Z | 355.524° N | 2025-10-19 04:35:26.459Z | 287.105° WNW | 31.696° | 2025-10-19 04:40:26.459Z | 230.415° WSW |
| 4 mins | 2025-10-19 12:51:26.459Z | 73.827° E | 2025-10-19 12:53:26.459Z | 52.087° ENE | 14.671° | 2025-10-19 12:55:26.459Z | 31.311° NE |
| 11 mins | 2025-10-19 14:30:26.459Z | 162.438° S | 2025-10-19 14:35:26.459Z | 352.69° N | 44.971° | 2025-10-19 14:41:26.459Z | 344.562° N |
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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