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: 10 hours ago
TLE from 10 hours ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 26221.64878053 .00001878 00000-0 16647-3 0 9997
2 59104 97.8459 352.5046 0005210 207.8300 152.2643 14.97444465132654Epoch: 2026-08-09T15:34Z
TLE epoch observation values (Epoch: 2026-08-09T15:34:14.637Z)
Latitude
-0.0001°
Longitude
160.80088°
Altitude
581.05 km
Speed
7.568 km/s
True Right ascension
23h 30m 01s
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
15:25:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.432 km
Perigee altitude
568.19 km
Semi-major axis
6,949.948 km
Eccentricity
0.00052
Inclination
97.8459°
RAAN
352.5046°
Arg. of periapsis
207.83°
True anomaly
152.29207°
Mean anomaly
152.2643°
Eccentric anomaly
152.27819°
Mean motion
3.74603 °/min
Orbital period
96.1 mins
BSTAR
0.00016647
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-10 07:45:50.886Z | 104.744° ESE | 2026-08-10 07:47:50.886Z | 74.213° E | 16.207° | 2026-08-10 07:50:50.886Z | 26.381° NE |
| 6 mins | 2026-08-10 09:20:50.886Z | 205.8° SW | 2026-08-10 09:22:50.886Z | 250.41° W | 30.428° | 2026-08-10 09:26:50.886Z | 329.437° NNW |
| 5 mins | 2026-08-10 21:01:50.886Z | 50.672° ENE | 2026-08-10 21:03:50.886Z | 94.358° ESE | 25.646° | 2026-08-10 21:06:50.886Z | 152.483° SSE |
| 4 mins | 2026-08-10 22:37:50.886Z | 314.609° NW | 2026-08-10 22:38:50.886Z | 294.314° NW | 19.621° | 2026-08-10 22:41:50.886Z | 244.506° 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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