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: 7 hours ago
TLE from 7 hours ago
0 PE2_FLT1 (TYVAK-0261)
1 59105U 24043H 26248.31073700 .00001828 00000-0 16184-3 0 9998
2 59105 97.8478 19.2299 0007454 125.1496 235.0425 14.97523013136641Epoch: 2026-09-05T07:27Z
TLE epoch observation values (Epoch: 2026-09-05T07:27:27.676Z)
Latitude
-0.00005°
Longitude
-77.05745°
Altitude
580.572 km
Speed
7.569 km/s
True Right ascension
01h 16m 55s
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
06:45:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.748 km
Perigee altitude
566.387 km
Semi-major axis
6,949.705 km
Eccentricity
0.00075
Inclination
97.8478°
RAAN
19.2299°
Arg. of periapsis
125.1496°
True anomaly
234.97253°
Mean anomaly
235.0425°
Eccentric anomaly
235.00751°
Mean motion
3.74622 °/min
Orbital period
96.1 mins
BSTAR
0.00016184
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-05 20:52:45.209Z | 55.051° ENE | 2026-09-05 20:54:45.209Z | 92.1° ESE | 20.254° | 2026-09-05 20:57:45.209Z | 143.753° SSE |
| 5 mins | 2026-09-05 22:27:45.209Z | 337.021° NNW | 2026-09-05 22:29:45.209Z | 297.924° NW | 24.106° | 2026-09-05 22:32:45.209Z | 238.633° WSW |
| 6 mins | 2026-09-06 09:14:45.209Z | 194.101° SSW | 2026-09-06 09:17:45.209Z | 273.722° WNW | 34.817° | 2026-09-06 09:20:45.209Z | 331.227° NNW |
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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