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: 18 hours ago

TLE from 18 hours ago
0 DELTA 1 R/B
1  3094U 68002B   25306.50252948 -.00000011  00000-0  21304-3 0  9999
2  3094 105.8013 177.8028 0312856  55.1433  15.5886 12.85265812710837
Epoch: 2025-11-02T12:03Z
TLE epoch observation values (Epoch: 2025-11-02T12:03:38.547Z)
Latitude
66.11781°
Longitude
-84.60874°
Altitude
1,099.983 km
Speed
7.418 km/s
True Right ascension
09h 13m 16s
True Declination
65° 59' 46"
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
02:08:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,558.931 km
Perigee altitude
1,077.365 km
Semi-major axis
7,696.285 km
Eccentricity
0.03129
Inclination
105.8013°
RAAN
177.8028°
Arg. of periapsis
55.1433°
True anomaly
16.58961°
Mean anomaly
15.5886°
Eccentric anomaly
16.08525°
Mean motion
3.21456 °/min
Orbital period
111.99 mins
BSTAR
0.00021304
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