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: 9 hours ago

TLE from 9 hours ago
0 DELTA 1 R/B
1 02096U 66016B   26075.17276625  .00000005  00000-0  23807-3 0  9990
2 02096 100.8853 277.8104 0039820 354.0909 119.2029 12.69993069782268
Epoch: 2026-03-16T04:08Z
TLE epoch observation values (Epoch: 2026-03-16T04:08:47.003Z)
Latitude
64.14512°
Longitude
-114.89675°
Altitude
1,408.054 km
Speed
7.155 km/s
True Right ascension
08h 04m 16s
True Declination
64° 01' 16"
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
17:59:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.33 km
Perigee altitude
1,348.549 km
Semi-major axis
7,757.576 km
Eccentricity
0.00398
Inclination
100.8853°
RAAN
277.8104°
Arg. of periapsis
354.0909°
True anomaly
119.60024°
Mean anomaly
119.2029°
Eccentric anomaly
119.40167°
Mean motion
3.17654 °/min
Orbital period
113.33 mins
BSTAR
0.00023807
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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