DELTA 4 R/B, 41746

Orbit data source: Space-Track

DELTA 4 R/B, 41746 is space debris in GEO originally from a launch on Fri, 19 Aug 2016 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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DELTA 4 R/B details

Identifier	41746, 2016-052C
Orbit	GEO
Last TLE update	12 hours ago
Origin	ULA (US)
Manufacturer	ULA Decatur
Mission	2))"
Bus & Motor	DCSS-4, RL10B-2
Mass	2,850 kg wet, 2,850 kg dry
Launch date (UTC)	2016-08-19 (8 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl + 1 Nozzle, Unknown HBR
Radar Cross Section	43.982 m²

Expand to show TLE details & history

TLE from 12 hours ago

0 DELTA 4 R/B
1 41746U 16052C   24361.18795439  .00000037  00000-0  00000-0 0  9998
2 41746   7.4329  62.9748 0005524 313.4882  46.3519  0.98990504 20352

Epoch: 2024-12-26T04:30Z

Definitive object data (Epoch: 2024-12-26T04:30:39.259Z)

Latitude	-0°
Longitude	-99.97767°
Altitude	36,132.978 km
Speed	3.063 km/s
True Right ascension	04h 11m 25s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	0.19656°
Longitude	78.51277°
Altitude	36,165.767 km
Speed	3.06 km/s
Apparent Right ascension	16h 06m 49s
Apparent Declination	-5° 57' 05"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	15:54:21
Azimuth	175.688° S
Elevation	44.043°
Doppler factor	1

Orbital elements

Apogee altitude	36,174.182 km
Perigee altitude	36,127.196 km
Semi-major axis	42,528.826 km
Eccentricity	0.0005524
Inclination	7.4329°
RAAN	62.9748°
Arg. of periapsis	313.4882°
True anomaly	46.39773°
Mean anomaly	46.3519°
Eccentric anomaly	46.37481°
Mean motion	0.24747 °/min
BSTAR	Unknown
Orbital period	1454.74 mins