DELTA 1 DEB, 2976

Orbit data source: Space-Track

DELTA 1 DEB, 2976 is space debris in SSO originally from a launch on Thu, 20 Apr 1967 UTC launched from the Air Force Western Test Range (AFWTR). 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
2976, 1967-036C
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1967-04-20 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1 02976U 67036C   26154.64416983 -.00000030  00000-0  89108-4 0  9999
2 02976 102.1751 310.5251 0098813 145.8225 276.8210 12.82105959765978
Epoch: 2026-06-03T15:27Z
TLE epoch observation values (Epoch: 2026-06-03T15:27:36.273Z)
Latitude
59.32031°
Longitude
165.3103°
Altitude
1,334.567 km
Speed
7.2 km/s
True Right ascension
19h 17m 14s
True Declination
59° 10' 50"
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
09:27:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,406.716 km
Perigee altitude
1,254.373 km
Semi-major axis
7,708.682 km
Eccentricity
0.00988
Inclination
102.1751°
RAAN
310.5251°
Arg. of periapsis
145.8225°
True anomaly
275.69512°
Mean anomaly
276.821°
Eccentric anomaly
276.25822°
Mean motion
3.20681 °/min
Orbital period
112.26 mins
BSTAR
0.000089108
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Other satellites on launch #36 in the year 1967 (1967-04-20 UTC)

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