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: 10 hours ago

TLE from 10 hours ago
0 DELTA 1 R/B
1   979U 65004B   26193.55102650  .00000054  00000-0  87262-4 0  9993
2   979  96.4138  38.0732 1138296 206.7069 147.0776 12.15534697718642
Epoch: 2026-07-12T13:13Z
TLE epoch observation values (Epoch: 2026-07-12T13:13:28.689Z)
Latitude
-0.00005°
Longitude
-90.7446°
Altitude
2,404.98 km
Speed
6.396 km/s
True Right ascension
02h 32m 17s
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
11:51:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,518.563 km
Perigee altitude
700.138 km
Semi-major axis
7,987.487 km
Eccentricity
0.11383
Inclination
96.4138°
RAAN
38.0732°
Arg. of periapsis
206.7069°
True anomaly
153.39532°
Mean anomaly
147.0776°
Eccentric anomaly
150.30815°
Mean motion
3.04038 °/min
Orbital period
118.41 mins
BSTAR
0.000087262
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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