DELTA 1 R/B, 575
Orbit data source: Space-Track
DELTA 1 R/B, 575 is space debris in HEO originally from a launch on Tue, 07 May 1963 UTC launched from the Air Force Eastern Test Range (AFETR). 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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Edit Public Description
Identifier | |
Orbit | HEO |
Last TLE update | 14 hours ago |
Origin | |
Manufacturer | ABL |
Mission | Spacecraft |
Bus & Motor | ALTAIR, Unknown motor |
Mass | 24 kg wet, 24 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 1.52 m |
Radar Cross Section | 0.695 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 14 hours ago
0 DELTA 1 R/B
1 00575U 63013B 25075.22207362 -.00000038 00000-0 -33394-3 0 9991
2 00575 42.7721 50.3389 4006780 16.1100 359.7624 6.40253933446650
Epoch: 2025-03-16T05:19Z
Definitive object data (Epoch: 2025-03-16T05:19:47.16Z)
Latitude | 10.48211° |
Longitude | 167.80829° |
Altitude | 963.264 km |
Speed | 8.722 km/s |
True Right ascension | 04h 07m 14s |
True Declination | 10° 25' 21" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -41.48642° |
Longitude | 83.46084° |
Altitude | 4,184.22 km |
Speed | 6.557 km/s |
Apparent Right ascension | 20h 16m 18s |
Apparent Declination | -68° 23' 29" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 00:27:36 |
Azimuth | 201.754° SSW |
Elevation | -27.877° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 10,783.419 km |
Perigee altitude | 964.948 km |
Semi-major axis | 12,252.321 km |
Eccentricity | 0.400678 |
Inclination | 42.7721° |
RAAN | 50.3389° |
Arg. of periapsis | 16.11° |
True anomaly | 359.39393° |
Mean anomaly | 359.7624° |
Eccentric anomaly | 359.60355° |
Mean motion | 1.60035 °/min |
BSTAR | -0.00033394 |
Orbital period | 224.95 mins |
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Other satellites on launch #13 in the year 1963 (1963-05-07 UTC)
TELSTAR 2 (A-41), 573 |
DELTA 1 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. |
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11 mins | 2025-03-17 00:07:28.353Z | 179.452° S | 2025-03-17 00:11:28.353Z | 131.981° SE | 22.686° | 2025-03-17 00:18:28.353Z | 78.024° E |
39 mins | 2025-03-17 04:00:28.353Z | 269.673° W | 2025-03-17 04:08:28.353Z | 9.524° NNE | 44.597° | 2025-03-17 04:39:28.353Z | 88° E |
89 mins | 2025-03-17 07:56:28.353Z | 289.913° WNW | 2025-03-17 08:15:28.353Z | 210.913° SW | 43.168° | 2025-03-17 09:25:28.353Z | 144.727° SSE |
71 mins | 2025-03-17 12:03:28.353Z | 275.983° WNW | 2025-03-17 12:29:28.353Z | 242.525° WSW | 19.858° | 2025-03-17 13:14:28.353Z | 209.067° SW |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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