DELTA 1 R/B, 979

Orbit data source: Space-Track

DELTA 1 R/B, 979 is space debris in SSO originally from a launch on Fri, 22 Jan 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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Identifier
979, 1965-004B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
1965-01-22 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 DELTA 1 R/B
1 00979U 65004B   26036.75046416  .00000078  00000-0  11364-3 0  9993
2 00979  96.4336 316.6472 1138668 188.1233 169.9905 12.15490989699591
Epoch: 2026-02-05T18:00Z
TLE epoch observation values (Epoch: 2026-02-05T18:00:40.103Z)
Latitude
0.00005°
Longitude
-89.41811°
Altitude
2,513.773 km
Speed
6.309 km/s
True Right ascension
21h 06m 35s
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
15:22:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,519.074 km
Perigee altitude
700.011 km
Semi-major axis
7,987.679 km
Eccentricity
0.11387
Inclination
96.4336°
RAAN
316.6472°
Arg. of periapsis
188.1233°
True anomaly
171.97812°
Mean anomaly
169.9905°
Eccentric anomaly
171.00997°
Mean motion
3.04027 °/min
Orbital period
118.41 mins
BSTAR
0.00011364
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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