DELTA 4 R/B, 40535
Orbit data source: Space-Track
DELTA 4 R/B, 40535 is space debris in MEO originally from a launch on Wed, 25 Mar 2015 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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40535 intel report (Beta)
DELTA 4 R/B details
| Identifier | |
| Orbit | MEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | ULA Decatur |
| Mission | 2))" |
| Bus & Motor | DCSS-4, RL10B-2 |
| Mass | 2,850 kg wet, 2,850 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl + 1 Nozzle, Unknown HBR |
| Radar Cross Section | 43.982 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 DELTA 4 R/B
1 40535U 15013B 24347.10281867 .00000031 00000-0 00000-0 0 9994
2 40535 52.8214 237.4033 0034082 57.6430 302.7591 1.92974522 68502Epoch: 2024-12-12T02:28Z
Definitive object data (Epoch: 2024-12-12T02:28:03.533Z)
| Latitude | -0.00003° |
| Longitude | 119.10342° |
| Altitude | 20,824.275 km |
| Speed | 3.832 km/s |
| True Right ascension | 15h 49m 37s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 15.77762° |
| Longitude | -73.29072° |
| Altitude | 20,893.51 km |
| Speed | 3.822 km/s |
| Apparent Right ascension | 02h 18m 24s |
| Apparent Declination | 7° 43' 15" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 07:20:20 |
| Azimuth | 266.638° W |
| Elevation | 16.065° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 20,967.057 km |
| Perigee altitude | 20,781.294 km |
| Semi-major axis | 27,252.312 km |
| Eccentricity | 0.0034082 |
| Inclination | 52.8214° |
| RAAN | 237.4033° |
| Arg. of periapsis | 57.643° |
| True anomaly | 302.42991° |
| Mean anomaly | 302.7591° |
| Eccentric anomaly | 302.59458° |
| Mean motion | 0.48243 °/min |
| BSTAR | Unknown |
| Orbital period | 746.22 mins |
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Other satellites on launch #13 in the year 2015 (2015-03-25 UTC)
| NAVSTAR 73 (USA 260), 40534 |
| DELTA 4 R/B, 40535 |
| DELTA 4 DEB, 40597 (Decayed) |
| DELTA 4 DEB, 40598 (Decayed) |
| DELTA 4 DEB, 40599 (Decayed) |
| DELTA 4 DEB, 40649 |
DELTA 4 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. |
|---|---|---|---|---|---|---|---|
| 27 mins | 2024-12-13 08:50:40.079Z | 266.613° W | 2024-12-13 08:50:40.079Z | 266.613° W | 15.459° | 2024-12-13 09:17:40.079Z | 256.812° W |
| 309 mins | 2024-12-13 14:43:40.079Z | 160.756° S | 2024-12-13 17:17:40.079Z | 94.484° ESE | 40.203° | 2024-12-13 19:52:40.079Z | 51.658° ENE |
| 47 mins | 2024-12-14 08:03:40.079Z | 313.252° NW | 2024-12-14 08:33:40.079Z | 301.963° NW | 11.634° | 2024-12-14 08:50:40.079Z | 295.3° NW |
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