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
Last TLE update
12 hours ago
Origin
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
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 12 hours ago
0 DELTA 1 R/B
1 03094U 68002B   25199.47986817 -.00000035  00000-0  13800-3 0  9992
2 03094 105.8157  27.2323 0313664 229.4371 188.3267 12.85255804697080
Epoch: 2025-07-18T11:31Z
TLE epoch observation values (Epoch: 2025-07-18T11:31:00.609Z)
Latitude
54.12631°
Longitude
-104.9936°
Altitude
1,568.044 km
Speed
6.978 km/s
True Right ascension
00h 17m 09s
True Declination
53° 58' 46"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
52.14637°
Longitude
119.89219°
Altitude
1,378.434 km
Speed
7.151 km/s
Apparent Right ascension
19h 41m 23s
Apparent Declination
26° 02' 02"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
11:53:03
Azimuth
53.17° ENE
Elevation
-1.842°
Doppler factor
1
Orbital elements
Apogee altitude
1,559.595 km
Perigee altitude
1,076.783 km
Semi-major axis
7,696.326 km
Eccentricity
0.03137
Inclination
105.8157°
RAAN
27.2323°
Arg. of periapsis
229.4371°
True anomaly
187.82565°
Mean anomaly
188.3267°
Eccentric anomaly
188.07428°
Mean motion
3.21453 °/min
Orbital period
111.99 mins
BSTAR
0.000138
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