DELTA 2 R/B, 25637
Orbit data source: Space-Track
DELTA 2 R/B, 25637 is space debris in SSO originally from a launch on Tue, 23 Feb 1999 UTC launched from the Air Force Western Test Range (AFWTR). 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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25637 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 DELTA 2 R/B
1 25637U 99008D 26154.62618937 .00000362 00000-0 92557-4 0 9992
2 25637 96.4827 54.0182 0135352 294.2270 128.5433 14.49276341438794Epoch: 2026-06-03T15:01Z
TLE epoch observation values (Epoch: 2026-06-03T15:01:42.761Z)
Latitude
63.32063°
Longitude
-76.49096°
Altitude
799.667 km
Speed
7.428 km/s
True Right ascension
02h 44m 04s
True Declination
63° 10' 59"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:11:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
821.18 km
Perigee altitude
628.894 km
Semi-major axis
7,103.174 km
Eccentricity
0.01354
Inclination
96.4827°
RAAN
54.0182°
Arg. of periapsis
294.227°
True anomaly
129.74366°
Mean anomaly
128.5433°
Eccentric anomaly
129.14475°
Mean motion
3.62547 °/min
Orbital period
99.3 mins
BSTAR
0.000092557
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Other satellites on launch #8 in the year 1999 (1999-02-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DELTA 2 R/B Visibility forecast
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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 | 2026-06-05 16:34:45.564Z | 127.593° SE | 2026-06-05 16:38:45.564Z | 61.606° ENE | 27.996° | 2026-06-05 16:42:45.564Z | 9.657° NNE |
| 7 mins | 2026-06-05 18:13:45.564Z | 218.399° SW | 2026-06-05 18:16:45.564Z | 266.447° W | 25.062° | 2026-06-05 18:20:45.564Z | 323.15° NNW |
| 4 mins | 2026-06-06 04:40:45.564Z | 70.53° E | 2026-06-06 04:41:45.564Z | 82.714° E | 13.761° | 2026-06-06 04:44:45.564Z | 118.056° SE |
| 9 mins | 2026-06-06 06:16:45.564Z | 3.742° NNE | 2026-06-06 06:20:45.564Z | 306.067° NW | 42.595° | 2026-06-06 06:25:45.564Z | 202.554° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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