PE2_FLT1 (TYVAK-0261), 59105
Orbit data source: Space-Track
PE2_FLT1 (TYVAK-0261), 59105 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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59105 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: 9 hours ago
TLE from 9 hours ago
0 PE2_FLT1 (TYVAK-0261)
1 59105U 24043H 26125.27825926 .00002853 00000-0 25288-3 0 9996
2 59105 97.8321 255.8264 0006119 172.5566 187.5748 14.97018799118233Epoch: 2026-05-05T06:40Z
TLE epoch observation values (Epoch: 2026-05-05T06:40:41.600Z)
Latitude
0.00007°
Longitude
-67.50234°
Altitude
583.379 km
Speed
7.566 km/s
True Right ascension
17h 03m 18s
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
23:29:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.382 km
Perigee altitude
568.875 km
Semi-major axis
6,951.266 km
Eccentricity
0.00061
Inclination
97.8321°
RAAN
255.8264°
Arg. of periapsis
172.5566°
True anomaly
187.56556°
Mean anomaly
187.5748°
Eccentric anomaly
187.57018°
Mean motion
3.74496 °/min
Orbital period
96.13 mins
BSTAR
0.00025288
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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_FLT1 (TYVAK-0261) 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 | 2026-05-05 21:40:24.724Z | 8.577° NNE | 2026-05-05 21:44:24.724Z | 248.597° W | 43.556° | 2026-05-05 21:47:24.724Z | 200.336° SSW |
| 6 mins | 2026-05-06 08:29:24.724Z | 148.142° SSE | 2026-05-06 08:31:24.724Z | 93.972° ESE | 41.12° | 2026-05-06 08:35:24.724Z | 355.157° N |
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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