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
CYL, 2.6 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 DELTA 1 R/B
1 03616U 68114B   26244.48715825 -.00000032  00000-0  81598-4 0  9995
2 03616 101.6898 189.3143 0012998 237.4461 236.3815 12.51403517638145
Epoch: 2026-09-01T11:41Z
TLE epoch observation values (Epoch: 2026-09-01T11:41:30.472Z)
Latitude
63.80694°
Longitude
-121.97287°
Altitude
1,475.092 km
Speed
7.129 km/s
True Right ascension
02h 16m 13s
True Declination
63° 40' 59"
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
10:23:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,466.354 km
Perigee altitude
1,445.988 km
Semi-major axis
7,834.308 km
Eccentricity
0.0013
Inclination
101.6898°
RAAN
189.3143°
Arg. of periapsis
237.4461°
True anomaly
236.25758°
Mean anomaly
236.3815°
Eccentric anomaly
236.31953°
Mean motion
3.12998 °/min
Orbital period
115.02 mins
BSTAR
0.000081598
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