DELTA 4 R/B, 36412

Orbit data source: Space-Track

DELTA 4 R/B, 36412 is space debris in HEO originally from a launch on Thu, 04 Mar 2010 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	36412, 2010-008B
Orbit	HEO
Last TLE update	17 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)	2010-03-04 (15 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, Large (>1 m²)

Expand to show TLE details & history

TLE from 17 hours ago

0 DELTA 4 R/B
1 36412U 10008B   24325.71260910 -.00000181  00000-0  00000-0 0  9998
2 36412  12.4294  68.5209 5262174 333.3792 264.9510  1.92896677103643

Epoch: 2024-11-20T17:06Z

Definitive object data (Epoch: 2024-11-20T17:06:09.426Z)

Latitude	-1.81637°
Longitude	-60.02078°
Altitude	28,284.777 km
Speed	2.894 km/s
True Right ascension	17h 06m 53s
True Declination	-1° 48' 51"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	9.0137°
Longitude	157.49136°
Altitude	10,666.674 km
Speed	5.67 km/s
Apparent Right ascension	07h 59m 03s
Apparent Declination	-6° 36' 51"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	06:41:41
Azimuth	154.497° SSE
Elevation	40.163°
Doppler factor	1

Orbital elements

Apogee altitude	35,229.619 km
Perigee altitude	6,538.13 km
Semi-major axis	27,262.012 km
Eccentricity	0.5262174
Inclination	12.4294°
RAAN	68.5209°
Arg. of periapsis	333.3792°
True anomaly	215.04907°
Mean anomaly	264.951°
Eccentric anomaly	239.0845°
Mean motion	0.48218 °/min
BSTAR	Unknown
Orbital period	746.61 mins