DELTA 1 R/B(2), 1318

Orbit data source: Space-Track

DELTA 1 R/B(2), 1318 is space debris in HEO originally from a launch on Tue, 06 Apr 1965 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 1 R/B(2) details

Identifier	1318, 1965-028B
Orbit	HEO
Last TLE update	17 hours ago
Origin	GSFC (US)
Manufacturer	ABL
Mission	Spacecraft
Bus & Motor	ALTAIR, Unknown motor
Mass	33 kg wet, 33 kg dry
Launch date (UTC)	1965-04-06 (60 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 1.5 m
Radar Cross Section	0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 17 hours ago

0 DELTA 1 R/B(2)
1  1318U 65028B   24361.28470894 -.00000244  00000-0  00000+0 0  9992
2  1318  18.1220  52.1200 6952329 239.0503  44.9589  2.11830878247164

Epoch: 2024-12-26T06:49Z

Definitive object data (Epoch: 2024-12-26T06:49:58.852Z)

Latitude	2.85513°
Longitude	-136.86356°
Altitude	17,613.869 km
Speed	4.203 km/s
True Right ascension	04h 03m 35s
True Declination	2° 51' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	17.41322°
Longitude	-72.72276°
Altitude	34,079.831 km
Speed	2.035 km/s
Apparent Right ascension	08h 40m 06s
Apparent Declination	10° 48' 34"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	23:33:02
Azimuth	48.132° ENE
Elevation	-25.375°
Doppler factor	1

Orbital elements

Apogee altitude	37,043.458 km
Perigee altitude	1,428.149 km
Semi-major axis	25,613.941 km
Eccentricity	0.6952329
Inclination	18.122°
RAAN	52.12°
Arg. of periapsis	239.0503°
True anomaly	130.04463°
Mean anomaly	44.9589°
Eccentric anomaly	84.61715°
Mean motion	0.52945 °/min
BSTAR	Unknown
Orbital period	679.95 mins