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 (27 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: 7 hours ago

TLE from 7 hours ago
0 DELTA 2 R/B
1 25876U 99041E   26306.39219830  .00000388  00000-0  10095-3 0  9990
2 25876  51.7636  71.4788 0500092 330.2092  27.1205 14.12293135396611
Epoch: 2026-11-02T09:24Z
TLE epoch observation values (Epoch: 2026-11-02T09:24:45.933Z)
Latitude
-0.00004°
Longitude
-111.38249°
Altitude
534.49 km
Speed
7.761 km/s
True Right ascension
04h 45m 54s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
12:14:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,213.569 km
Perigee altitude
490.423 km
Semi-major axis
7,230.133 km
Eccentricity
0.05001
Inclination
51.7636°
RAAN
71.4788°
Arg. of periapsis
330.2092°
True anomaly
29.88533°
Mean anomaly
27.1205°
Eccentric anomaly
28.48715°
Mean motion
3.5304 °/min
Orbital period
101.97 mins
BSTAR
0.00010095
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Other satellites on launch #41 in the year 1999 (1999-07-25 UTC)

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