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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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: 8 hours ago
TLE from 8 hours ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 26235.61434117 .00001612 00000-0 14350-3 0 9993
2 59104 97.8467 6.5278 0006173 167.8048 192.3324 14.97488424134745Epoch: 2026-08-23T14:44Z
TLE epoch observation values (Epoch: 2026-08-23T14:44:39.077Z)
Latitude
-0.00001°
Longitude
173.45711°
Altitude
581.9 km
Speed
7.567 km/s
True Right ascension
00h 26m 06s
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
14:00:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.965 km
Perigee altitude
567.385 km
Semi-major axis
6,949.812 km
Eccentricity
0.00062
Inclination
97.8467°
RAAN
6.5278°
Arg. of periapsis
167.8048°
True anomaly
192.3173°
Mean anomaly
192.3324°
Eccentric anomaly
192.32485°
Mean motion
3.74614 °/min
Orbital period
96.1 mins
BSTAR
0.0001435
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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 | 2026-08-24 08:31:03.117Z | 146.858° SSE | 2026-08-24 08:34:03.117Z | 75.992° E | 38.7° | 2026-08-24 08:37:03.117Z | 1.427° NNE |
| 6 mins | 2026-08-24 21:48:03.117Z | 7.061° NNE | 2026-08-24 21:50:03.117Z | 289.928° WNW | 44.514° | 2026-08-24 21:54:03.117Z | 197.639° SSW |
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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