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: 7 hours ago

TLE from 7 hours ago
0 DELTA 1 R/B
1  3094U 68002B   26189.41355409 -.00000060  00000-0  51740-4 0  9997
2  3094 105.8069 166.4109 0313607  11.8317 140.3819 12.85288149742686
Epoch: 2026-07-08T09:55Z
TLE epoch observation values (Epoch: 2026-07-08T09:55:31.073Z)
Latitude
24.55996°
Longitude
-81.44159°
Altitude
1,511.778 km
Speed
7.023 km/s
True Right ascension
23h 35m 13s
True Declination
24° 26' 33"
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
04:47:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,559.418 km
Perigee altitude
1,076.701 km
Semi-major axis
7,696.197 km
Eccentricity
0.03136
Inclination
105.8069°
RAAN
166.4109°
Arg. of periapsis
11.8317°
True anomaly
142.60567°
Mean anomaly
140.3819°
Eccentric anomaly
141.50045°
Mean motion
3.21461 °/min
Orbital period
111.99 mins
BSTAR
0.00005174
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