DELTA 1 R/B, 4354
Orbit data source: Space-Track
DELTA 1 R/B, 4354 is space debris in HEO originally from a launch on Fri, 20 Mar 1970 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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4354 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | HEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | Thiokol/TE |
| Mission | Spacecraft |
| Bus & Motor | STAR 37, Unknown motor |
| Mass | 65 kg wet, 65 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Sphere + Cone, 1 m |
| Radar Cross Section | 0.734 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 DELTA 1 R/B
1 04354U 70021B 25070.42183798 .00002908 00000-0 11479-2 0 9995
2 04354 25.3187 252.5339 6327376 332.3208 4.8745 3.53229590362072Epoch: 2025-03-11T10:07Z
Definitive object data (Epoch: 2025-03-11T10:07:26.801Z)
| Latitude | 0.0004° |
| Longitude | -68.64444° |
| Altitude | 631.078 km |
| Speed | 9.584 km/s |
| True Right ascension | 16h 50m 10s |
| True Declination | 0° 00' 01" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 2.50664° |
| Longitude | 105.38121° |
| Altitude | 20,371.044 km |
| Speed | 2.814 km/s |
| Apparent Right ascension | 04h 16m 48s |
| Apparent Declination | -5° 16' 10" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 15:24:45 |
| Azimuth | 337.898° N |
| Elevation | -53.424° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 23,363.891 km |
| Perigee altitude | 311.933 km |
| Semi-major axis | 18,216.049 km |
| Eccentricity | 0.6327376 |
| Inclination | 25.3187° |
| RAAN | 252.5339° |
| Arg. of periapsis | 332.3208° |
| True anomaly | 27.1728° |
| Mean anomaly | 4.8745° |
| Eccentric anomaly | 13.07741° |
| Mean motion | 0.8828 °/min |
| BSTAR | 0.0011479 |
| Orbital period | 407.79 mins |
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Other satellites on launch #21 in the year 1970 (1970-03-20 UTC)
| NATO 2A, 4353 |
| DELTA 1 DEB, 5975 |
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. |
|---|---|---|---|---|---|---|---|
| 26 mins | 2025-03-12 13:25:50.105Z | 150.097° SSE | 2025-03-12 13:32:50.105Z | 116.19° SE | 15.995° | 2025-03-12 13:51:50.105Z | 86.385° E |
| 331 mins | 2025-03-12 20:30:50.105Z | 265.519° W | 2025-03-12 21:45:50.105Z | 212.327° SW | 41.016° | 2025-03-13 02:01:50.105Z | 168.935° S |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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