DELTA 1 R/B, 3616

Orbit data source: Space-Track

DELTA 1 R/B, 3616 is space debris in SSO originally from a launch on Sun, 15 Dec 1968 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
3616, 1968-114B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Aerojet
Mission
Spacecraft
Bus & Motor
ABLESTAR, Unknown motor
Mass
~785 kg wet, ~785 kg dry
Launch date (UTC)
1968-12-15 (58 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 DELTA 1 R/B
1  3616U 68114B   26171.41891068 -.00000025  00000-0  12700-3 0  9991
2  3616 101.6851 117.6405 0013722  20.1749  98.2424 12.51402387629001
Epoch: 2026-06-20T10:03Z
TLE epoch observation values (Epoch: 2026-06-20T10:03:13.882Z)
Latitude
59.40942°
Longitude
-101.42842°
Altitude
1,470.082 km
Speed
7.133 km/s
True Right ascension
21h 12m 03s
True Declination
59° 16' 20"
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
23:27:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,466.926 km
Perigee altitude
1,445.426 km
Semi-major axis
7,834.313 km
Eccentricity
0.00137
Inclination
101.6851°
RAAN
117.6405°
Arg. of periapsis
20.1749°
True anomaly
98.39798°
Mean anomaly
98.2424°
Eccentric anomaly
98.32019°
Mean motion
3.12998 °/min
Orbital period
115.02 mins
BSTAR
0.000127
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