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: 5 hours ago

TLE from 5 hours ago
0 DELTA 1 R/B
1 03094U 68002B   25351.64466521 -.00000030  00000-0  15257-3 0  9999
2 03094 105.7991 241.2770 0314185 341.7026  86.9472 12.85273181716635
Epoch: 2025-12-17T15:28Z
TLE epoch observation values (Epoch: 2025-12-17T15:28:19.074Z)
Latitude
66.49674°
Longitude
-117.66015°
Altitude
1,326.194 km
Speed
7.203 km/s
True Right ascension
13h 23m 43s
True Declination
66° 22' 48"
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
18:58:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,559.924 km
Perigee altitude
1,076.314 km
Semi-major axis
7,696.256 km
Eccentricity
0.03142
Inclination
105.7991°
RAAN
241.277°
Arg. of periapsis
341.7026°
True anomaly
90.54755°
Mean anomaly
86.9472°
Eccentric anomaly
88.74692°
Mean motion
3.21458 °/min
Orbital period
111.99 mins
BSTAR
0.00015257
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