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: 19 hours ago
TLE from 19 hours ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 26079.35419162 .00002547 00000-0 22810-3 0 9991
2 59104 97.8244 209.8767 0005444 348.7440 11.3659 14.96716345111364Epoch: 2026-03-20T08:30Z
TLE epoch observation values (Epoch: 2026-03-20T08:30:02.155Z)
Latitude
-0.00002°
Longitude
-95.52274°
Altitude
576.384 km
Speed
7.575 km/s
True Right ascension
13h 59m 30s
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
08:11:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.85 km
Perigee altitude
570.281 km
Semi-major axis
6,952.203 km
Eccentricity
0.00054
Inclination
97.8244°
RAAN
209.8767°
Arg. of periapsis
348.744°
True anomaly
11.3782°
Mean anomaly
11.3659°
Eccentric anomaly
11.37205°
Mean motion
3.7442 °/min
Orbital period
96.15 mins
BSTAR
0.0002281
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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
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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 | 2026-03-21 08:41:20.820Z | 169.017° S | 2026-03-21 08:44:20.820Z | 183.443° SSW | 43.021° | 2026-03-21 08:48:20.820Z | 345.834° N |
| 6 mins | 2026-03-21 21:58:20.820Z | 352.502° N | 2026-03-21 22:01:20.820Z | 280.682° WNW | 34.106° | 2026-03-21 22:04:20.820Z | 219.943° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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