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: 13 hours ago
TLE from 13 hours ago
0 PE2_FLT1 (TYVAK-0261)
1 59105U 24043H 26286.59583223 .00003073 00000-0 26750-3 0 9990
2 59105 97.8557 57.7041 0006245 20.0558 340.0908 14.97675407142375Epoch: 2026-10-13T14:17Z
TLE epoch observation values (Epoch: 2026-10-13T14:17:59.904Z)
Latitude
-0.00003°
Longitude
-178.95314°
Altitude
573.045 km
Speed
7.577 km/s
True Right ascension
03h 50m 48s
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
22:04:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.436 km
Perigee altitude
566.756 km
Semi-major axis
6,949.233 km
Eccentricity
0.00062
Inclination
97.8557°
RAAN
57.7041°
Arg. of periapsis
20.0558°
True anomaly
340.06641°
Mean anomaly
340.0908°
Eccentric anomaly
340.07861°
Mean motion
3.7466 °/min
Orbital period
96.09 mins
BSTAR
0.0002675
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-14 08:05:01.869Z | 117.743° SE | 2026-10-14 08:08:01.869Z | 62.021° ENE | 23.925° | 2026-10-14 08:11:01.869Z | 14.848° NNE |
| 5 mins | 2026-10-14 09:41:01.869Z | 226.402° WSW | 2026-10-14 09:43:01.869Z | 269.242° W | 24.567° | 2026-10-14 09:46:01.869Z | 318.895° NNW |
| 6 mins | 2026-10-14 21:21:01.869Z | 36.171° NE | 2026-10-14 21:23:01.869Z | 79.288° E | 41.403° | 2026-10-14 21:27:01.869Z | 169.84° S |
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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