DELTA 4 DEB, 40649

Orbit data source: Space-Track

DELTA 4 DEB, 40649 is space debris in HEO originally from a launch on Wed, 25 Mar 2015 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
40649, 2015-013F
Orbit
HEO
Country
Flag of USUS
Related business
Flag of USUnited Launch Alliance/Lockheed Martin (US)
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2015-03-25 (11 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 DELTA 4 DEB
1 40649U 15013F   25348.53860298  .00000036  00000-0  00000-0 0  9995
2 40649  52.1718 194.2023 5581562 169.2273 211.1710  3.87530405  4396
Epoch: 2025-12-14T12:55Z
TLE epoch observation values (Epoch: 2025-12-14T12:55:35.297Z)
Latitude
-0.00002°
Longitude
-83.13728°
Altitude
19,715.798 km
Speed
2.697 km/s
True Right ascension
12h 56m 50s
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
02:44:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,299.657 km
Perigee altitude
1,186.841 km
Semi-major axis
17,121.386 km
Eccentricity
0.55816
Inclination
52.1718°
RAAN
194.2023°
Arg. of periapsis
169.2273°
True anomaly
190.81153°
Mean anomaly
211.171°
Eccentric anomaly
200.15299°
Mean motion
0.9688 °/min
Orbital period
371.59 mins
BSTAR
0
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