DELTA 1 R/B, 2096

Orbit data source: Space-Track

DELTA 1 R/B, 2096 is space debris in SSO originally from a launch on Mon, 28 Feb 1966 UTC launched from the Air Force Eastern Test Range (AFETR). 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
2096, 1966-016B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1966-02-28 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
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: 5 hours ago

TLE from 5 hours ago
0 DELTA 1 R/B
1  2096U 66016B   26035.84133631 -.00000021  00000-0  10481-3 0  9992
2  2096 100.8860 240.5836 0040123  74.7121 297.4878 12.69990744777278
Epoch: 2026-02-04T20:11Z
TLE epoch observation values (Epoch: 2026-02-04T20:11:31.457Z)
Latitude
11.53521°
Longitude
160.46212°
Altitude
1,369.585 km
Speed
7.182 km/s
True Right ascension
15h 53m 22s
True Declination
11° 28' 24"
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
03:04:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.575 km
Perigee altitude
1,348.323 km
Semi-major axis
7,757.586 km
Eccentricity
0.00401
Inclination
100.886°
RAAN
240.5836°
Arg. of periapsis
74.7121°
True anomaly
297.07899°
Mean anomaly
297.4878°
Eccentric anomaly
297.28349°
Mean motion
3.17653 °/min
Orbital period
113.33 mins
BSTAR
0.00010481
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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