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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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: 13 hours ago
TLE from 13 hours ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 26286.86196981 .00002961 00000-0 25793-3 0 9991
2 59104 97.8570 58.0284 0006405 23.2476 336.9034 14.97684692142419Epoch: 2026-10-13T20:41Z
TLE epoch observation values (Epoch: 2026-10-13T20:41:14.191Z)
Latitude
-0.00005°
Longitude
85.29932°
Altitude
573.003 km
Speed
7.577 km/s
True Right ascension
03h 52m 06s
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
04:25:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.518 km
Perigee altitude
566.617 km
Semi-major axis
6,949.205 km
Eccentricity
0.00064
Inclination
97.857°
RAAN
58.0284°
Arg. of periapsis
23.2476°
True anomaly
336.87459°
Mean anomaly
336.9034°
Eccentric anomaly
336.889°
Mean motion
3.74663 °/min
Orbital period
96.09 mins
BSTAR
0.00025793
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-14 21:18:37.638Z | 30.857° NE | 2026-10-14 21:21:37.638Z | 87.482° E | 40.503° | 2026-10-14 21:25:37.638Z | 169.298° S |
| 4 mins | 2026-10-15 08:07:37.638Z | 103.826° ESE | 2026-10-15 08:09:37.638Z | 59.534° ENE | 24.423° | 2026-10-15 08:11:37.638Z | 23.313° NE |
| 5 mins | 2026-10-15 09:42:37.638Z | 228.72° WSW | 2026-10-15 09:44:37.638Z | 271.426° WNW | 23.722° | 2026-10-15 09:47:37.638Z | 319.173° 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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