DELTA 1 DEB, 1313
Orbit data source: Space-Track
DELTA 1 DEB, 1313 is space debris in SSO originally from a launch on Fri, 22 Jan 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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1313 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 DELTA 1 DEB
1 01313U 65004D 25299.64229413 .00000393 00000-0 59308-3 0 9994
2 01313 96.4211 353.0029 1174472 101.3675 272.1398 12.00804907658411Epoch: 2025-10-26T15:24Z
TLE epoch observation values (Epoch: 2025-10-26T15:24:54.212Z)
Latitude
0.00003°
Longitude
86.52145°
Altitude
1,755.35 km
Speed
6.969 km/s
True Right ascension
23h 32m 00s
True Declination
0° 00' 00"
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
16:10:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,620.346 km
Perigee altitude
728.809 km
Semi-major axis
8,052.715 km
Eccentricity
0.11745
Inclination
96.4211°
RAAN
353.0029°
Arg. of periapsis
101.3675°
True anomaly
258.73986°
Mean anomaly
272.1398°
Eccentric anomaly
265.43195°
Mean motion
3.00351 °/min
Orbital period
119.86 mins
BSTAR
0.00059308
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Other satellites on launch #4 in the year 1965 (1965-01-22 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 DEB 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-01 03:28:56.332Z | 165.338° S | 2025-11-01 03:35:56.332Z | 20.059° NNE | 44.581° | 2025-11-01 03:39:56.332Z | 351.307° N |
| 10 mins | 2025-11-01 15:58:56.332Z | 24.357° NE | 2025-11-01 16:01:56.332Z | 79.499° E | 41.83° | 2025-11-01 16:08:56.332Z | 180.776° SSW |
| 4 mins | 2025-11-01 17:59:56.332Z | 302.097° NW | 2025-11-01 18:00:56.332Z | 290.517° WNW | 14.287° | 2025-11-01 18:03:56.332Z | 261.73° 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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