DELTA 1 R/B, 1433
Orbit data source: Space-Track
DELTA 1 R/B, 1433 is space debris in SSO originally from a launch on Fri, 02 Jul 1965 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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1433 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | SSO |
| Last TLE update | 15 hours ago |
| Origin | |
| Manufacturer | ABL |
| Mission | Spacecraft |
| Bus & Motor | ALTAIR, Unknown motor |
| Mass | 60 kg wet, 60 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 15 hours ago
0 DELTA 1 R/B
1 01433U 65051B 25081.47463932 .00004778 00000-0 96722-3 0 9997
2 01433 98.5108 220.6343 0039047 232.9137 126.8491 14.61311535128826Epoch: 2025-03-22T11:23Z
Definitive object data (Epoch: 2025-03-22T11:23:28.837Z)
| Latitude | -0.00002° |
| Longitude | -130.45504° |
| Altitude | 708.541 km |
| Speed | 7.493 km/s |
| True Right ascension | 14h 42m 32s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -4.73301° |
| Longitude | -129.11623° |
| Altitude | 708.138 km |
| Speed | 7.493 km/s |
| Apparent Right ascension | 16h 33m 16s |
| Apparent Declination | -24° 44' 42" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 07:12:23 |
| Azimuth | 77.69° E |
| Elevation | -53.505° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 713.62 km |
| Perigee altitude | 658.453 km |
| Semi-major axis | 7,064.173 km |
| Eccentricity | 0.0039047 |
| Inclination | 98.5108° |
| RAAN | 220.6343° |
| Arg. of periapsis | 232.9137° |
| True anomaly | 127.20611° |
| Mean anomaly | 126.8491° |
| Eccentric anomaly | 127.02771° |
| Mean motion | 3.65554 °/min |
| BSTAR | 0.00096722 |
| Orbital period | 98.48 mins |
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Other satellites on launch #51 in the year 1965 (1965-07-02 UTC)
| TIROS 10, 1430 |
| DELTA 1 DEB, 1440 (Decayed) |
| DELTA 1 DEB, 1529 |
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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-03-23 08:52:34.174Z | 150.902° SSE | 2025-03-23 08:56:34.174Z | 77.51° E | 41.122° | 2025-03-23 09:00:34.174Z | 356.068° N |
| 7 mins | 2025-03-23 22:29:34.174Z | 354.886° N | 2025-03-23 22:32:34.174Z | 266.984° W | 38.321° | 2025-03-23 22:36:34.174Z | 211.292° SW |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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