TRANSIT 11 DEB, 11991
Orbit data source: Space-Track
TRANSIT 11 DEB, 11991 is space debris in LEO originally from a launch on Fri, 28 Jan 1966 UTC launched from the Air Force Western Test Range (AFWTR). 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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11991 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
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: 17 hours ago
TLE from 17 hours ago
0 TRANSIT 11 DEB
1 11991U 66005H 25258.50852090 .00000628 00000-0 48794-3 0 9990
2 11991 90.1716 337.6847 0177748 103.8919 320.0734 13.84364973983388Epoch: 2025-09-15T12:12Z
TLE epoch observation values (Epoch: 2025-09-15T12:12:16.205Z)
Latitude
62.72389°
Longitude
159.57396°
Altitude
860.394 km
Speed
7.478 km/s
True Right ascension
22h 29m 24s
True Declination
62° 35' 08"
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
21:50:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.619 km
Perigee altitude
815.269 km
Semi-major axis
7,323.581 km
Eccentricity
0.01777
Inclination
90.1716°
RAAN
337.6847°
Arg. of periapsis
103.8919°
True anomaly
318.74362°
Mean anomaly
320.0734°
Eccentric anomaly
319.41078°
Mean motion
3.46304 °/min
Orbital period
103.95 mins
BSTAR
0.00048794
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Other satellites on launch #5 in the year 1966 (1966-01-28 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.TRANSIT 11 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-16 05:21:57.485Z | 158.655° S | 2025-09-16 05:26:57.485Z | 74.23° E | 40.188° | 2025-09-16 05:31:57.485Z | 6.626° NNE |
| 5 mins | 2025-09-16 07:08:57.485Z | 254.895° W | 2025-09-16 07:10:57.485Z | 279.425° WNW | 16.642° | 2025-09-16 07:13:57.485Z | 314.534° NW |
| 9 mins | 2025-09-16 17:58:57.485Z | 354.511° N | 2025-09-16 18:02:57.485Z | 295.18° NW | 42.212° | 2025-09-16 18:07:57.485Z | 195.964° SSW |
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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