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: 15 hours ago
TLE from 15 hours ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 25293.85238794 .00006141 00000-0 56487-3 0 9994
2 59104 97.8140 59.6280 0007845 119.6799 240.5204 14.95107337 88863Epoch: 2025-10-20T20:27Z
TLE epoch observation values (Epoch: 2025-10-20T20:27:26.318Z)
Latitude
0.00007°
Longitude
83.21958°
Altitude
587.775 km
Speed
7.565 km/s
True Right ascension
03h 58m 30s
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
06:33:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.514 km
Perigee altitude
573.599 km
Semi-major axis
6,957.193 km
Eccentricity
0.00078
Inclination
97.814°
RAAN
59.628°
Arg. of periapsis
119.6799°
True anomaly
240.44218°
Mean anomaly
240.5204°
Eccentric anomaly
240.48129°
Mean motion
3.74018 °/min
Orbital period
96.25 mins
BSTAR
0.00056487
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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
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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 21:06:55.846Z | 22.65° NE | 2025-10-21 21:10:55.846Z | 126.135° SE | 38.658° | 2025-10-21 21:13:55.846Z | 177.368° S |
| 5 mins | 2025-10-22 07:56:55.846Z | 119.773° SE | 2025-10-22 07:58:55.846Z | 71.029° E | 28.908° | 2025-10-22 08:01:55.846Z | 11.601° NNE |
| 4 mins | 2025-10-22 09:32:55.846Z | 240.972° WSW | 2025-10-22 09:33:55.846Z | 258.43° W | 16.839° | 2025-10-22 09:36:55.846Z | 307.482° NW |
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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