DRAGRACER 2(AUGURY), 46955
Orbit data source: Space-Track
DRAGRACER 2(AUGURY), 46955 is a payload satellite owned by TriSept (US) in SSO that was launched on Fri, 20 Nov 2020 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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46955 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Millenium ES
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 DRAGRACER 2(AUGURY)
1 46955U 20085AC 26165.09978344 .00038367 00000-0 30825-3 0 9996
2 46955 97.5791 1.0351 0003376 266.3039 93.7837 15.70890438311385Epoch: 2026-06-14T02:23Z
TLE epoch observation values (Epoch: 2026-06-14T02:23:41.289Z)
Latitude
-0.00001°
Longitude
62.70769°
Altitude
359.656 km
Speed
7.693 km/s
True Right ascension
00h 04m 08s
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
22:45:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
355.529 km
Perigee altitude
350.984 km
Semi-major axis
6,731.394 km
Eccentricity
0.00034
Inclination
97.5791°
RAAN
1.0351°
Arg. of periapsis
266.3039°
True anomaly
93.8223°
Mean anomaly
93.7837°
Eccentric anomaly
93.803°
Mean motion
3.92994 °/min
Orbital period
91.6 mins
BSTAR
0.00030825
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Other satellites on launch #85 in the year 2020 (2020-11-20 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.DRAGRACER 2(AUGURY) 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-14 13:13:48.267Z | 175.919° S | 2026-06-14 13:15:48.267Z | 230.069° WSW | 42.406° | 2026-06-14 13:17:48.267Z | 339.411° N |
| 4 mins | 2026-06-15 01:53:48.267Z | 22.337° NNE | 2026-06-15 01:54:48.267Z | 45.043° ENE | 40.028° | 2026-06-15 01:57:48.267Z | 186.203° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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