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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 DRAGRACER 2(AUGURY)
1 46955U 20085AC 26234.99319714 .00042781 00000-0 27547-3 0 9994
2 46955 97.5750 77.0953 0004197 33.5469 326.6061 15.76066774322376Epoch: 2026-08-22T23:50Z
TLE epoch observation values (Epoch: 2026-08-22T23:50:12.232Z)
Latitude
-0.00004°
Longitude
108.2487°
Altitude
342.403 km
Speed
7.705 km/s
True Right ascension
05h 08m 22s
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
15:00:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
341.315 km
Perigee altitude
335.677 km
Semi-major axis
6,716.633 km
Eccentricity
0.00042
Inclination
97.575°
RAAN
77.0953°
Arg. of periapsis
33.5469°
True anomaly
326.57962°
Mean anomaly
326.6061°
Eccentric anomaly
326.59286°
Mean motion
3.9429 °/min
Orbital period
91.3 mins
BSTAR
0.00027547
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-24 02:17:26.333Z | 21.015° NNE | 2026-08-24 02:20:26.333Z | 148.129° SSE | 36.101° | 2026-08-24 02:22:26.333Z | 181.056° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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