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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2096 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 DELTA 1 R/B
1 2096U 66016B 25289.15917720 .00000000 00000-0 21273-3 0 9992
2 2096 100.8940 134.8460 0039753 305.3601 171.2229 12.69983636763094Epoch: 2025-10-16T03:49Z
TLE epoch observation values (Epoch: 2025-10-16T03:49:12.910Z)
Latitude
61.44822°
Longitude
-106.77329°
Altitude
1,422.864 km
Speed
7.141 km/s
True Right ascension
22h 21m 48s
True Declination
61° 18' 57"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:05:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.317 km
Perigee altitude
1,348.639 km
Semi-major axis
7,757.615 km
Eccentricity
0.00398
Inclination
100.894°
RAAN
134.846°
Arg. of periapsis
305.3601°
True anomaly
171.29207°
Mean anomaly
171.2229°
Eccentric anomaly
171.25752°
Mean motion
3.17651 °/min
Orbital period
113.33 mins
BSTAR
0.00021273
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DELTA 1 R/B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-10-16 12:46:13.795Z | 133.508° SE | 2025-10-16 12:53:13.795Z | 69.645° E | 35.939° | 2025-10-16 13:00:13.795Z | 357.035° N |
| 13 mins | 2025-10-16 14:39:13.795Z | 202.56° SW | 2025-10-16 14:45:13.795Z | 265.838° W | 31.466° | 2025-10-16 14:52:13.795Z | 327.792° NNW |
| 14 mins | 2025-10-17 02:31:13.795Z | 22.382° NNE | 2025-10-17 02:38:13.795Z | 118.037° SE | 43.285° | 2025-10-17 02:45:13.795Z | 187.323° SSW |
| 10 mins | 2025-10-17 04:24:13.795Z | 344.95° N | 2025-10-17 04:28:13.795Z | 308.392° NW | 24.112° | 2025-10-17 04:34:13.795Z | 254.841° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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