TYVAK-0172, 46267
Orbit data source: Space-Track
TYVAK-0172, 46267 is a payload satellite owned by Echostar AU (US) in SSO 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Tyvak NSS
Mission
Operational 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 day ago
TLE from 1 day ago
0 TYVAK-0172
1 46267U 20059C 26006.18315175 .00061333 00000-0 10114-2 0 9991
2 46267 97.7264 243.2171 0002318 93.0879 267.0638 15.52093558293382Epoch: 2026-01-06T04:23Z
TLE epoch observation values (Epoch: 2026-01-06T04:23:44.311Z)
Latitude
0.00001°
Longitude
71.51285°
Altitude
413.82 km
Speed
7.663 km/s
True Right ascension
16h 12m 52s
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
11:22:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
409.125 km
Perigee altitude
405.979 km
Semi-major axis
6,785.689 km
Eccentricity
0.00023
Inclination
97.7264°
RAAN
243.2171°
Arg. of periapsis
93.0879°
True anomaly
267.03727°
Mean anomaly
267.0638°
Eccentric anomaly
267.05054°
Mean motion
3.88286 °/min
Orbital period
92.72 mins
BSTAR
0.0010114
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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 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 | 2026-01-07 16:06:23.540Z | 194.327° SSW | 2026-01-07 16:09:23.540Z | 277.618° WNW | 29.324° | 2026-01-07 16:11:23.540Z | 324.931° NNW |
| 4 mins | 2026-01-08 04:55:23.540Z | 347.959° N | 2026-01-08 04:57:23.540Z | 275.709° WNW | 33.154° | 2026-01-08 04:59:23.540Z | 220.202° SW |
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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