DELTA 1 DEB, 2706

Orbit data source: Space-Track

DELTA 1 DEB, 2706 is space debris in SSO originally from a launch on Thu, 26 Jan 1967 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
2706, 1967-006C
Orbit
SSO
Last TLE update
2 days ago
Origin
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1967-01-26 (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
Small (<0.1 m²)

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TLE from 2 days ago
0 DELTA 1 DEB
1  2706U 67006C   25198.55081931 -.00000045  00000-0  21991-4 0  9997
2  2706 102.2131 219.7485 0035175 339.6097 171.9821 12.60921089690823
Epoch: 2025-07-17T13:13Z
TLE epoch observation values (Epoch: 2025-07-17T13:13:10.788Z)
Latitude
27.69516°
Longitude
-87.66998°
Altitude
1,449.407 km
Speed
7.127 km/s
True Right ascension
03h 04m 57s
True Declination
27° 33' 59"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
2.3479°
Longitude
-91.49955°
Altitude
1,446.887 km
Speed
7.127 km/s
Apparent Right ascension
01h 29m 29s
Apparent Declination
-49° 09' 12"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
03:42:06
Azimuth
201.006° SSW
Elevation
-3.752°
Doppler factor
1
Orbital elements
Apogee altitude
1,444.124 km
Perigee altitude
1,389.287 km
Semi-major axis
7,794.842 km
Eccentricity
0.00352
Inclination
102.2131°
RAAN
219.7485°
Arg. of periapsis
339.6097°
True anomaly
172.03808°
Mean anomaly
171.9821°
Eccentric anomaly
172.01011°
Mean motion
3.15379 °/min
Orbital period
114.15 mins
BSTAR
0.000021991
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