DELTA 4 R/B, 29156
Orbit data source: Space-Track
DELTA 4 R/B, 29156 is space debris in HEO originally from a launch on Wed, 24 May 2006 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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29156 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 day ago
0 DELTA 4 R/B
1 29156U 06018B 25174.28122483 -.00000295 00000-0 00000-0 0 9994
2 29156 13.2652 309.0651 5251611 313.8498 6.3470 1.93076821134538
Epoch: 2025-06-23T06:44Z
TLE epoch observation values (Epoch: 2025-06-23T06:44:57.825Z)
Latitude
-5.08039°
Longitude
-85.94872°
Altitude
6,905.352 km
Speed
6.737 km/s
True Right ascension
19h 07m 56s
True Declination
-5° 03' 51"
Sunlit
Visualization orbit readout
Latitude
3.57106°
Longitude
100.64538°
Altitude
29,788.881 km
Speed
2.722 km/s
Apparent Right ascension
08h 03m 36s
Apparent Declination
-3° 03' 16"
Sunlit
Visualization observer readout
Local Sidereal Time
03:23:52
Azimuth
105.534° ESE
Elevation
13.214°
Doppler factor
1
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Other satellites on launch #18 in the year 2006 (2006-05-24 UTC)
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. |
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44 mins | 2025-06-24 16:12:04.883Z | 105.551° ESE | 2025-06-24 16:12:04.883Z | 105.551° ESE | 12.868° | 2025-06-24 16:56:04.883Z | 107.57° ESE |
470 mins | 2025-06-25 08:22:04.883Z | 203.361° SW | 2025-06-25 08:54:04.883Z | 145.041° SSE | 24.767° | 2025-06-25 16:12:04.883Z | 112.728° SE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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