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
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 DELTA 1 R/B
1 02096U 66016B   25258.51437601 -.00000025  00000-0  84059-4 0  9993
2 02096 100.8998 105.8117 0040241   8.4535 105.1434 12.69981396759208
Epoch: 2025-09-15T12:20Z
TLE epoch observation values (Epoch: 2025-09-15T12:20:42.087Z)
Latitude
63.82372°
Longitude
128.86157°
Altitude
1,401.14 km
Speed
7.161 km/s
True Right ascension
20h 35m 01s
True Declination
63° 41' 55"
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
20:19:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.705 km
Perigee altitude
1,348.27 km
Semi-major axis
7,757.625 km
Eccentricity
0.00402
Inclination
100.8998°
RAAN
105.8117°
Arg. of periapsis
8.4535°
True anomaly
105.58793°
Mean anomaly
105.1434°
Eccentric anomaly
105.36572°
Mean motion
3.17651 °/min
Orbital period
113.33 mins
BSTAR
0.000084059
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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