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: 1 day ago
TLE from 1 day ago
0 PE2_FLT1 (TYVAK-0261)
1 59105U 24043H 25341.29471747 .00017587 00000-0 15832-2 0 9998
2 59105 97.8159 106.9206 0004583 328.6429 31.4518 14.95667414 95956Epoch: 2025-12-07T07:04Z
TLE epoch observation values (Epoch: 2025-12-07T07:04:23.589Z)
Latitude
-0°
Longitude
-75.48785°
Altitude
580.627 km
Speed
7.572 km/s
True Right ascension
07h 07m 40s
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
05:45:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.506 km
Perigee altitude
574.13 km
Semi-major axis
6,955.455 km
Eccentricity
0.00046
Inclination
97.8159°
RAAN
106.9206°
Arg. of periapsis
328.6429°
True anomaly
31.47922°
Mean anomaly
31.4518°
Eccentric anomaly
31.46551°
Mean motion
3.74158 °/min
Orbital period
96.22 mins
BSTAR
0.0015832
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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
Loading observer location...
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 | 2025-12-08 08:52:36.148Z | 184.064° SSW | 2025-12-08 08:56:36.148Z | 275.018° WNW | 37.56° | 2025-12-08 08:59:36.148Z | 333.939° NNW |
| 4 mins | 2025-12-08 20:36:36.148Z | 68.685° E | 2025-12-08 20:37:36.148Z | 88.944° E | 20.521° | 2025-12-08 20:40:36.148Z | 142.015° SSE |
| 5 mins | 2025-12-08 22:11:36.148Z | 325.824° NNW | 2025-12-08 22:13:36.148Z | 278.34° WNW | 24.268° | 2025-12-08 22:16:36.148Z | 232.124° WSW |
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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