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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1 03127U 68002D   26176.89673515 -.00000050  00000-0  80607-4 0  9996
2 03127 105.3267 328.4291 0321672 290.1158 228.2098 12.84893809740087
Epoch: 2026-06-25T21:31Z
TLE epoch observation values (Epoch: 2026-06-25T21:31:17.916Z)
Latitude
23.45461°
Longitude
-81.63272°
Altitude
1,493.642 km
Speed
7.041 km/s
True Right ascension
10h 20m 53s
True Declination
23° 20' 28"
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
13:06:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,567.212 km
Perigee altitude
1,071.983 km
Semi-major axis
7,697.735 km
Eccentricity
0.03217
Inclination
105.3267°
RAAN
328.4291°
Arg. of periapsis
290.1158°
True anomaly
225.53425°
Mean anomaly
228.2098°
Eccentric anomaly
226.86485°
Mean motion
3.21365 °/min
Orbital period
112.02 mins
BSTAR
0.000080607
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