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
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1967-01-26 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.050 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 02706U 67006C   26305.12029000 -.00000050  00000-0 -72718-5 0  9991
2 02706 102.1572 350.4350 0035537 154.5046 231.0999 12.60935771749816
Epoch: 2026-11-01T02:53Z
TLE epoch observation values (Epoch: 2026-11-01T02:53:13.055Z)
Latitude
24.71046°
Longitude
-98.94674°
Altitude
1,439.232 km
Speed
7.136 km/s
True Right ascension
22h 59m 05s
True Declination
24° 35' 29"
Sunlit
Object was in full shadow 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
03:02:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,444.342 km
Perigee altitude
1,388.941 km
Semi-major axis
7,794.778 km
Eccentricity
0.00355
Inclination
102.1572°
RAAN
350.435°
Arg. of periapsis
154.5046°
True anomaly
230.78386°
Mean anomaly
231.0999°
Eccentric anomaly
230.94179°
Mean motion
3.15382 °/min
Orbital period
114.15 mins
BSTAR
-0.0000072718
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Other satellites on launch #6 in the year 1967 (1967-01-26 UTC)

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