DELTA 1 R/B(2), 1318
Orbit data source: Space-Track
DELTA 1 R/B(2), 1318 is space debris in HEO originally from a launch on Tue, 06 Apr 1965 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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1318 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: 13 hours ago
TLE from 13 hours ago
0 DELTA 1 R/B(2)
1 01318U 65028B 25293.20396307 -.00000187 00000-0 00000-0 0 9992
2 01318 18.0532 331.5567 6940351 29.2661 65.0700 2.11819303102243Epoch: 2025-10-20T04:53Z
TLE epoch observation values (Epoch: 2025-10-20T04:53:42.409Z)
Latitude
2.31954°
Longitude
42.03984°
Altitude
23,422.668 km
Speed
3.345 km/s
True Right ascension
09h 37m 30s
True Declination
2° 18' 58"
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
13:10:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,014.334 km
Perigee altitude
1,459.111 km
Semi-major axis
25,614.859 km
Eccentricity
0.69404
Inclination
18.0532°
RAAN
331.5567°
Arg. of periapsis
29.2661°
True anomaly
143.08088°
Mean anomaly
65.07°
Eccentric anomaly
103.70337°
Mean motion
0.52943 °/min
Orbital period
679.98 mins
BSTAR
0
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Other satellites on launch #28 in the year 1965 (1965-04-06 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(2) 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. |
|---|---|---|---|---|---|---|---|
| 185 mins | 2025-10-20 18:13:37.017Z | 219.741° SW | 2025-10-20 18:13:37.017Z | 219.741° SW | 25.903° | 2025-10-20 21:18:37.017Z | 235.152° WSW |
| 297 mins | 2025-10-21 13:16:37.017Z | 251.157° W | 2025-10-21 14:08:37.017Z | 194.812° SSW | 35.142° | 2025-10-21 18:13:37.017Z | 206.593° SW |
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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