TYVAK-0172, 46267 (Decayed)
Orbit data source: Space-Track
TYVAK-0172, 46267 was a payload satellite owned by Echostar AU (US) in LEO that was launched on Sun, 30 Aug 2020 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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46267 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Tyvak NSS
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT 6U?, Unknown motor
Mass
11 kg wet, 11 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, Unknown HBR
Radar Cross Section
0.077 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 TYVAK-0172
1 46267U 20059C 26096.83989262 .14635205 28105-5 16297-2 0 9995
2 46267 97.7020 342.8884 0007965 229.9948 130.0651 16.37139113307583Epoch: 2026-04-06T20:09Z
TLE epoch observation values (Epoch: 2026-04-06T20:09:26.722Z)
Latitude
0.00003°
Longitude
-154.59814°
Altitude
180.024 km
Speed
7.796 km/s
True Right ascension
22h 51m 33s
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
17:43:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
175.465 km
Perigee altitude
165.033 km
Semi-major axis
6,548.386 km
Eccentricity
0.0008
Inclination
97.702°
RAAN
342.8884°
Arg. of periapsis
229.9948°
True anomaly
130.13491°
Mean anomaly
130.0651°
Eccentric anomaly
130.10001°
Mean motion
4.09583 °/min
Orbital period
87.89 mins
BSTAR
0.0016297
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Other satellites on launch #59 in the year 2020 (2020-08-30 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.TYVAK-0172 Visibility
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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. |
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| This satellite is decayed. |
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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