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: 11 hours ago

TLE from 11 hours ago
0 DELTA 1 R/B
1 02096U 66016B   25349.80593962 -.00000017  00000-0  12416-3 0  9997
2 02096 100.8864 192.2732 0039739 179.5160 246.0022 12.69987677770790
Epoch: 2025-12-15T19:20Z
TLE epoch observation values (Epoch: 2025-12-15T19:20:33.183Z)
Latitude
63.05406°
Longitude
155.32062°
Altitude
1,405.33 km
Speed
7.157 km/s
True Right ascension
11h 20m 37s
True Declination
62° 55' 35"
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
05:08:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.289 km
Perigee altitude
1,348.634 km
Semi-major axis
7,757.598 km
Eccentricity
0.00397
Inclination
100.8864°
RAAN
192.2732°
Arg. of periapsis
179.516°
True anomaly
245.58703°
Mean anomaly
246.0022°
Eccentric anomaly
245.79453°
Mean motion
3.17652 °/min
Orbital period
113.33 mins
BSTAR
0.00012416
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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