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 (62 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 DELTA 1 R/B
1   979U 65004B   26306.88955199  .00000117  00000-0  17017-3 0  9999
2   979  96.4182  96.8565 1137830 319.9107  32.3128 12.15555016732416
Epoch: 2026-11-02T21:20Z
TLE epoch observation values (Epoch: 2026-11-02T21:20:57.291Z)
Latitude
-0.00009°
Longitude
94.45771°
Altitude
880.587 km
Speed
7.745 km/s
True Right ascension
06h 27m 25s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
10:40:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,518.091 km
Perigee altitude
700.431 km
Semi-major axis
7,987.398 km
Eccentricity
0.11378
Inclination
96.4182°
RAAN
96.8565°
Arg. of periapsis
319.9107°
True anomaly
40.20328°
Mean anomaly
32.3128°
Eccentric anomaly
36.1594°
Mean motion
3.04043 °/min
Orbital period
118.4 mins
BSTAR
0.00017017
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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