PE2_FLT2 (TYVAK-0262), 59104
Orbit data source: Space-Track
PE2_FLT2 (TYVAK-0262), 59104 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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59104 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: 9 hours ago
TLE from 9 hours ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 25344.23823253 .00007071 00000-0 64024-3 0 9992
2 59104 97.8172 109.8671 0005570 325.1665 34.9190 14.95688734 96390Epoch: 2025-12-10T05:43Z
TLE epoch observation values (Epoch: 2025-12-10T05:43:03.290Z)
Latitude
-0.00008°
Longitude
-55.10803°
Altitude
580.103 km
Speed
7.572 km/s
True Right ascension
07h 19m 28s
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
13:11:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.126 km
Perigee altitude
573.378 km
Semi-major axis
6,955.389 km
Eccentricity
0.00056
Inclination
97.8172°
RAAN
109.8671°
Arg. of periapsis
325.1665°
True anomaly
34.95556°
Mean anomaly
34.919°
Eccentric anomaly
34.93728°
Mean motion
3.74163 °/min
Orbital period
96.21 mins
BSTAR
0.00064024
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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_FLT2 (TYVAK-0262) 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-10 20:44:59.277Z | 42.762° NE | 2025-12-10 20:47:59.277Z | 101.992° ESE | 25.292° | 2025-12-10 20:50:59.277Z | 154.017° SSE |
| 5 mins | 2025-12-10 22:20:59.277Z | 328.455° NNW | 2025-12-10 22:22:59.277Z | 290.642° WNW | 20.391° | 2025-12-10 22:25:59.277Z | 242.318° WSW |
| 5 mins | 2025-12-11 09:08:59.277Z | 209.827° SW | 2025-12-11 09:10:59.277Z | 255.095° W | 29.067° | 2025-12-11 09:13:59.277Z | 321.088° NNW |
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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