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
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 DELTA 1 R/B
1 00979U 65004B   25258.52578879  .00000087  00000-0  11660-3 0  9995
2 00979  96.4125 242.2416 1139945 139.9685 229.1316 12.15411595682192
Epoch: 2025-09-15T12:37Z
TLE epoch observation values (Epoch: 2025-09-15T12:37:08.151Z)
Latitude
-0.00003°
Longitude
58.22846°
Altitude
2,264.619 km
Speed
6.51 km/s
True Right ascension
16h 08m 57s
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
21:31:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,520.481 km
Perigee altitude
699.299 km
Semi-major axis
7,988.027 km
Eccentricity
0.11399
Inclination
96.4125°
RAAN
242.2416°
Arg. of periapsis
139.9685°
True anomaly
220.13489°
Mean anomaly
229.1316°
Eccentric anomaly
224.54964°
Mean motion
3.04007 °/min
Orbital period
118.42 mins
BSTAR
0.0001166
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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