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: 2 days ago
TLE from 2 days ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 26171.32849216 .00001766 00000-0 15770-3 0 9997
2 59104 97.8407 302.0141 0007098 44.0038 316.1747 14.97235890125128Epoch: 2026-06-20T07:53Z
TLE epoch observation values (Epoch: 2026-06-20T07:53:01.722Z)
Latitude
-0.00008°
Longitude
-84.78775°
Altitude
574.928 km
Speed
7.575 km/s
True Right ascension
20h 08m 03s
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
21:38:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.39 km
Perigee altitude
567.523 km
Semi-major axis
6,950.594 km
Eccentricity
0.00071
Inclination
97.8407°
RAAN
302.0141°
Arg. of periapsis
44.0038°
True anomaly
316.11834°
Mean anomaly
316.1747°
Eccentric anomaly
316.14652°
Mean motion
3.7455 °/min
Orbital period
96.12 mins
BSTAR
0.0001577
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 21:23:44.090Z | 20.564° NNE | 2026-06-22 21:27:44.090Z | 125.938° SE | 40.592° | 2026-06-22 21:30:44.090Z | 180.065° SSW |
| 5 mins | 2026-06-23 08:12:44.090Z | 124.029° SE | 2026-06-23 08:14:44.090Z | 76.419° E | 29.857° | 2026-06-23 08:17:44.090Z | 11.485° NNE |
| 4 mins | 2026-06-23 09:48:44.090Z | 241.428° WSW | 2026-06-23 09:49:44.090Z | 258.297° W | 15.648° | 2026-06-23 09:52:44.090Z | 306.393° NW |
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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