PE2_FLT1 (TYVAK-0261), 59105
Orbit data source: Space-Track
PE2_FLT1 (TYVAK-0261), 59105 is a payload satellite owned by Tyvak NSS (US) in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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59105 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Tyvak NSS
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
26 kg wet, 26 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.7 m
Radar Cross Section
0.149 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 PE2_FLT1 (TYVAK-0261)
1 59105U 24043H 26079.88920530 .00002957 00000-0 26397-3 0 9995
2 59105 97.8232 210.3915 0005129 342.3245 17.7797 14.96715281111447Epoch: 2026-03-20T21:20Z
TLE epoch observation values (Epoch: 2026-03-20T21:20:27.337Z)
Latitude
-0.00005°
Longitude
71.85981°
Altitude
576.703 km
Speed
7.574 km/s
True Right ascension
14h 01m 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
12:34:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.635 km
Perigee altitude
570.503 km
Semi-major axis
6,952.206 km
Eccentricity
0.00051
Inclination
97.8232°
RAAN
210.3915°
Arg. of periapsis
342.3245°
True anomaly
17.79766°
Mean anomaly
17.7797°
Eccentric anomaly
17.78868°
Mean motion
3.7442 °/min
Orbital period
96.15 mins
BSTAR
0.00026397
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.PE2_FLT1 (TYVAK-0261) 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-21 08:41:51.602Z | 169.579° S | 2026-03-21 08:44:51.602Z | 203.502° SW | 44.418° | 2026-03-21 08:48:51.602Z | 345.837° N |
| 6 mins | 2026-03-21 21:58:51.602Z | 350.2° N | 2026-03-21 22:01:51.602Z | 270.351° WNW | 33.282° | 2026-03-21 22:04:51.602Z | 218.725° 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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