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: 22 hours ago
TLE from 22 hours ago
0 DRAGRACER 2(AUGURY)
1 46955U 20085AC 26078.04606126 .00030630 00000-0 31430-3 0 9998
2 46955 97.5840 267.0082 0004879 233.3570 126.7241 15.64882493297742Epoch: 2026-03-19T01:06Z
TLE epoch observation values (Epoch: 2026-03-19T01:06:19.692Z)
Latitude
-0.00002°
Longitude
73.82505°
Altitude
378.694 km
Speed
7.681 km/s
True Right ascension
17h 48m 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
03:54:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
373.784 km
Perigee altitude
367.198 km
Semi-major axis
6,748.628 km
Eccentricity
0.00049
Inclination
97.584°
RAAN
267.0082°
Arg. of periapsis
233.357°
True anomaly
126.7689°
Mean anomaly
126.7241°
Eccentric anomaly
126.7465°
Mean motion
3.91489 °/min
Orbital period
91.96 mins
BSTAR
0.0003143
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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 | 2026-03-20 12:32:59.438Z | 161.695° S | 2026-03-20 12:33:59.438Z | 151.126° SSE | 40.784° | 2026-03-20 12:36:59.438Z | 350.211° N |
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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