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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Edit Public Description
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 25292.22146025 .00042248 00000-0 62859-3 0 9999
2 46955 97.5831 106.0064 0007759 80.5132 279.6998 15.55000008274230Epoch: 2025-10-19T05:18Z
TLE epoch observation values (Epoch: 2025-10-19T05:18:54.165Z)
Latitude
-0.00005°
Longitude
-1.66052°
Altitude
404.402 km
Speed
7.668 km/s
True Right ascension
07h 04m 01s
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
10:08:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
404.338 km
Perigee altitude
393.821 km
Semi-major axis
6,777.217 km
Eccentricity
0.00078
Inclination
97.5831°
RAAN
106.0064°
Arg. of periapsis
80.5132°
True anomaly
279.61215°
Mean anomaly
279.6998°
Eccentric anomaly
279.65597°
Mean motion
3.89015 °/min
Orbital period
92.54 mins
BSTAR
0.00062859
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-20 00:23:51.580Z | 20.81° NNE | 2025-10-20 00:26:51.580Z | 101.589° ESE | 39.854° | 2025-10-20 00:29:51.580Z | 180.812° 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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