THOR ALTAIR R/B, 1583
Orbit data source: Space-Track
THOR ALTAIR R/B, 1583 is space debris in SSO originally from a launch on Fri, 10 Sep 1965 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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1583 intel report (Beta)
THOR ALTAIR R/B details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | UTC |
| Mission | Spacecraft |
| Bus & Motor | FW4, Unknown motor |
| Mass | 25 kg wet, 25 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 1.5 m |
| Radar Cross Section | 0.687 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 THOR ALTAIR R/B
1 1583U 65072D 25017.55034401 .00002861 00000-0 49335-3 0 9998
2 1583 98.4559 235.5295 0146640 42.2896 318.9502 14.62492882112213Epoch: 2025-01-17T13:12Z
Definitive object data (Epoch: 2025-01-17T13:12:29.722Z)
| Latitude | -0.00001° |
| Longitude | -79.80671° |
| Altitude | 610.656 km |
| Speed | 7.595 km/s |
| True Right ascension | 15h 42m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 25.83128° |
| Longitude | -82.71517° |
| Altitude | 587.118 km |
| Speed | 7.623 km/s |
| Apparent Right ascension | 12h 05m 06s |
| Apparent Declination | -14° 52' 31" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 18:07:13 |
| Azimuth | 258.809° W |
| Elevation | -9.877° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 785.758 km |
| Perigee altitude | 578.692 km |
| Semi-major axis | 7,060.362 km |
| Eccentricity | 0.014664 |
| Inclination | 98.4559° |
| RAAN | 235.5295° |
| Arg. of periapsis | 42.2896° |
| True anomaly | 317.83129° |
| Mean anomaly | 318.9502° |
| Eccentric anomaly | 318.39229° |
| Mean motion | 3.6585 °/min |
| BSTAR | 0.00049335 |
| Orbital period | 98.4 mins |
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Other satellites on launch #72 in the year 1965 (1965-09-10 UTC)
| OPS 8068, 1580 |
| THOR ALTAIR DEB (YO), 1581 (Decayed) |
| THOR ALTAIR DEB (YO), 1582 (Decayed) |
| THOR ALTAIR R/B, 1583 |
| THOR ALTAIR DEB, 1931 |
| THOR ALTAIR DEB, 1932 (Decayed) |
THOR ALTAIR R/B 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-01-19 03:32:14.255Z | 4.623° NNE | 2025-01-19 03:35:14.255Z | 319.082° NNW | 41.51° | 2025-01-19 03:40:14.255Z | 204.915° SW |
| 6 mins | 2025-01-19 14:36:14.255Z | 182.905° SSW | 2025-01-19 14:38:14.255Z | 226.819° WSW | 40.452° | 2025-01-19 14:42:14.255Z | 338.747° N |
Authenticating...
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