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: 10 hours ago
TLE from 10 hours ago
0 PE2_FLT2 (TYVAK-0262)
1 59104U 24043G 26125.27810366 .00002930 00000-0 25968-3 0 9998
2 59104 97.8335 255.8540 0006162 176.6922 183.4341 14.97009705118234Epoch: 2026-05-05T06:40Z
TLE epoch observation values (Epoch: 2026-05-05T06:40:28.156Z)
Latitude
-0.00003°
Longitude
-67.41856°
Altitude
583.467 km
Speed
7.566 km/s
True Right ascension
17h 03m 24s
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
00:43:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.44 km
Perigee altitude
568.874 km
Semi-major axis
6,951.294 km
Eccentricity
0.00062
Inclination
97.8335°
RAAN
255.854°
Arg. of periapsis
176.6922°
True anomaly
183.42987°
Mean anomaly
183.4341°
Eccentric anomaly
183.43199°
Mean motion
3.74494 °/min
Orbital period
96.13 mins
BSTAR
0.00025968
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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 | 2026-05-05 21:40:55.756Z | 7.752° NNE | 2026-05-05 21:43:55.756Z | 290.515° WNW | 44.112° | 2026-05-05 21:47:55.756Z | 199.069° SSW |
| 6 mins | 2026-05-06 08:28:55.756Z | 149.444° SSE | 2026-05-06 08:31:55.756Z | 38.316° NE | 39.647° | 2026-05-06 08:34:55.756Z | 356.066° N |
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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