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: 2 days ago
TLE from 2 days ago
0 PE2_FLT1 (TYVAK-0261)
1 59105U 24043H 26171.32867097 .00001677 00000-0 14998-3 0 9997
2 59105 97.8394 301.9791 0006927 40.3168 319.8566 14.97226526125121Epoch: 2026-06-20T07:53Z
TLE epoch observation values (Epoch: 2026-06-20T07:53:17.171Z)
Latitude
-0.00004°
Longitude
-84.88731°
Altitude
574.836 km
Speed
7.575 km/s
True Right ascension
20h 07m 54s
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
21:49:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.3 km
Perigee altitude
567.671 km
Semi-major axis
6,950.623 km
Eccentricity
0.00069
Inclination
97.8394°
RAAN
301.9791°
Arg. of periapsis
40.3168°
True anomaly
319.80539°
Mean anomaly
319.8566°
Eccentric anomaly
319.831°
Mean motion
3.74548 °/min
Orbital period
96.12 mins
BSTAR
0.00014998
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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 | 2026-06-22 21:24:31.817Z | 22.043° NNE | 2026-06-22 21:27:31.817Z | 86.608° E | 41.297° | 2026-06-22 21:31:31.817Z | 182.057° SSW |
| 6 mins | 2026-06-23 08:12:31.817Z | 129.862° SE | 2026-06-23 08:15:31.817Z | 58.535° ENE | 29.669° | 2026-06-23 08:18:31.817Z | 7.384° NNE |
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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