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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Edit Public Description
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: 15 hours ago
TLE from 15 hours ago
0 PE2_FLT1 (TYVAK-0261)
1 59105U 24043H 25293.85249037 .00006325 00000-0 58155-3 0 9995
2 59105 97.8133 59.6214 0006730 112.9719 247.2212 14.95122181 88860Epoch: 2025-10-20T20:27Z
TLE epoch observation values (Epoch: 2025-10-20T20:27:35.167Z)
Latitude
-0.00006°
Longitude
83.17602°
Altitude
586.855 km
Speed
7.566 km/s
True Right ascension
03h 58m 29s
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
06:33:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.692 km
Perigee altitude
574.328 km
Semi-major axis
6,957.147 km
Eccentricity
0.00067
Inclination
97.8133°
RAAN
59.6214°
Arg. of periapsis
112.9719°
True anomaly
247.15012°
Mean anomaly
247.2212°
Eccentric anomaly
247.18566°
Mean motion
3.74021 °/min
Orbital period
96.25 mins
BSTAR
0.00058155
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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 | 2025-10-21 21:07:18.329Z | 23.519° NE | 2025-10-21 21:10:18.329Z | 77.051° E | 38.958° | 2025-10-21 21:14:18.329Z | 178.446° S |
| 5 mins | 2025-10-22 07:57:18.329Z | 116.036° SE | 2025-10-22 07:59:18.329Z | 62.826° ENE | 28.765° | 2025-10-22 08:02:18.329Z | 9.56° NNE |
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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