DELTA 2 R/B, 25876

Orbit data source: Space-Track

DELTA 2 R/B, 25876 is space debris in LEO originally from a launch on Sun, 25 Jul 1999 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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Identifier
25876, 1999-041E
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Boeing/HB
Mission
Spacecraft
Bus & Motor
DELTA/0020, Unknown motor
Mass
1,188 kg wet, 919 kg dry
Launch date (UTC)
1999-07-25 (26 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
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: 15 hours ago

TLE from 15 hours ago
0 DELTA 2 R/B
1 25876U 99041E   25258.11896647  .00000587  00000-0  13330-3 0  9998
2 25876  51.7623 282.0821 0505610 190.4496 168.5603 14.11115047338230
Epoch: 2025-09-15T02:51Z
TLE epoch observation values (Epoch: 2025-09-15T02:51:18.703Z)
Latitude
0.00001°
Longitude
-115.07402°
Altitude
1,215.408 km
Speed
7.066 km/s
True Right ascension
18h 48m 19s
True Declination
0° 00' 00"
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
10:03:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,221.785 km
Perigee altitude
490.253 km
Semi-major axis
7,234.156 km
Eccentricity
0.05056
Inclination
51.7623°
RAAN
282.0821°
Arg. of periapsis
190.4496°
True anomaly
169.6422°
Mean anomaly
168.5603°
Eccentric anomaly
169.10771°
Mean motion
3.52745 °/min
Orbital period
102.06 mins
BSTAR
0.0001333
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Other satellites on launch #41 in the year 1999 (1999-07-25 UTC)

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