DELTA 1 DEB, 3127

Orbit data source: Space-Track

DELTA 1 DEB, 3127 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
3127, 1968-002D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 DELTA 1 DEB
1  3127U 68002D   26083.52838346 -.00000044  00000-0  88682-4 0  9992
2  3127 105.3094 201.1351 0320646  87.3083 342.2993 12.84891751728094
Epoch: 2026-03-24T12:40Z
TLE epoch observation values (Epoch: 2026-03-24T12:40:52.330Z)
Latitude
63.87135°
Longitude
155.1879°
Altitude
1,098.048 km
Speed
7.42 km/s
True Right ascension
11h 09m 38s
True Declination
63° 44' 29"
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
00:10:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,566.43 km
Perigee altitude
1,072.78 km
Semi-major axis
7,697.742 km
Eccentricity
0.03206
Inclination
105.3094°
RAAN
201.1351°
Arg. of periapsis
87.3083°
True anomaly
341.13794°
Mean anomaly
342.2993°
Eccentric anomaly
341.72315°
Mean motion
3.21365 °/min
Orbital period
112.02 mins
BSTAR
0.000088682
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