DELTA 1 R/B, 3094

Orbit data source: Space-Track

DELTA 1 R/B, 3094 is space debris in LEO originally from a launch on Thu, 11 Jan 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
3094, 1968-002B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
~40 kg wet, ~40 kg dry
Launch date (UTC)
1968-01-11 (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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 DELTA 1 R/B
1  3094U 68002B   25321.44839177  .00000007  00000-0  27192-3 0  9999
2  3094 105.7998 198.8188 0313246  30.7879  49.5667 12.85268658712753
Epoch: 2025-11-17T10:45Z
TLE epoch observation values (Epoch: 2025-11-17T10:45:41.048Z)
Latitude
72.89565°
Longitude
-85.53774°
Altitude
1,180.647 km
Speed
7.341 km/s
True Right ascension
08h 50m 31s
True Declination
72° 48' 15"
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
15:43:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,559.22 km
Perigee altitude
1,077.054 km
Semi-major axis
7,696.274 km
Eccentricity
0.03132
Inclination
105.7998°
RAAN
198.8188°
Arg. of periapsis
30.7879°
True anomaly
52.36891°
Mean anomaly
49.5667°
Eccentric anomaly
50.96072°
Mean motion
3.21457 °/min
Orbital period
111.99 mins
BSTAR
0.00027192
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