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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Identifier
25637, 1999-008D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Boeing/HB
Mission
Spacecraft
Bus & Motor
DELTA/0020, Unknown motor
Mass
919 kg wet, 919 kg dry
Launch date (UTC)
1999-02-23 (27 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Cone, 3.0 m
Radar Cross Section
13.645 m², Large (>1 m²)

Expand to show TLE details & history
Last 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 14.49276341438794
Epoch: 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
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
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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