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: 10 hours ago
TLE from 10 hours ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 26034.15340268 .00004335 00000-0 38889-3 0 9990
2 59104 97.8187 164.6928 0007311 130.6280 229.5578 14.96262536104602Epoch: 2026-02-03T03:40Z
TLE epoch observation values (Epoch: 2026-02-03T03:40:53.991Z)
Latitude
-0.00002°
Longitude
-23.87058°
Altitude
584.805 km
Speed
7.566 km/s
True Right ascension
10h 58m 46s
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
15:32:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.556 km
Perigee altitude
570.388 km
Semi-major axis
6,953.609 km
Eccentricity
0.00073
Inclination
97.8187°
RAAN
164.6928°
Arg. of periapsis
130.628°
True anomaly
229.49408°
Mean anomaly
229.5578°
Eccentric anomaly
229.52594°
Mean motion
3.74307 °/min
Orbital period
96.18 mins
BSTAR
0.00038889
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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 | 2026-02-03 21:54:33.049Z | 351.579° N | 2026-02-03 21:57:33.049Z | 269.367° W | 34.155° | 2026-02-03 22:00:33.049Z | 217.178° SW |
| 6 mins | 2026-02-04 08:42:33.049Z | 173.635° S | 2026-02-04 08:44:33.049Z | 198.955° SSW | 42.748° | 2026-02-04 08:48:33.049Z | 344.152° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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