THOR ALTAIR DEB, 2177
Orbit data source: Space-Track
THOR ALTAIR DEB, 2177 is space debris in SSO originally from a launch on Thu, 31 Mar 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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2177 intel report (Beta)
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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 shape, 0.061 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 THOR ALTAIR DEB
1 02177U 66026D 26274.43984165 .00002135 00000-0 24717-3 0 9993
2 02177 98.9809 278.9192 0126082 15.8944 344.6166 14.81271658178571Epoch: 2026-10-01T10:33Z
TLE epoch observation values (Epoch: 2026-10-01T10:33:22.318Z)
Latitude
-0.00002°
Longitude
110.40009°
Altitude
543.227 km
Speed
7.637 km/s
True Right ascension
18h 35m 40s
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
04:48:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
710.667 km
Perigee altitude
534.139 km
Semi-major axis
7,000.54 km
Eccentricity
0.01261
Inclination
98.9809°
RAAN
278.9192°
Arg. of periapsis
15.8944°
True anomaly
344.22742°
Mean anomaly
344.6166°
Eccentric anomaly
344.42261°
Mean motion
3.70549 °/min
Orbital period
97.15 mins
BSTAR
0.00024717
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Other satellites on launch #26 in the year 1966 (1966-03-31 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.THOR ALTAIR 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-02 13:03:42.511Z | 26.43° NE | 2026-10-02 13:06:42.511Z | 74.863° E | 53.235° | 2026-10-02 13:11:42.511Z | 180.333° SSW |
| 5 mins | 2026-10-02 23:59:42.511Z | 128.571° SE | 2026-10-03 00:01:42.511Z | 64.147° ENE | 43.713° | 2026-10-03 00:04:42.511Z | 2.512° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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