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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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 PE2_FLT1 (TYVAK-0261)
1 59105U 24043H 26033.35095166 .00004074 00000-0 36587-3 0 9999
2 59105 97.8178 163.8759 0006422 125.1302 235.0522 14.96257994104481Epoch: 2026-02-02T08:25Z
TLE epoch observation values (Epoch: 2026-02-02T08:25:22.223Z)
Latitude
0.00001°
Longitude
-95.01419°
Altitude
584.078 km
Speed
7.567 km/s
True Right ascension
10h 55m 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
13:53:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.952 km
Perigee altitude
571.021 km
Semi-major axis
6,953.623 km
Eccentricity
0.00064
Inclination
97.8178°
RAAN
163.8759°
Arg. of periapsis
125.1302°
True anomaly
234.99191°
Mean anomaly
235.0522°
Eccentric anomaly
235.02205°
Mean motion
3.74306 °/min
Orbital period
96.18 mins
BSTAR
0.00036587
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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
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 | 2026-02-03 21:54:26.250Z | 352.871° N | 2026-02-03 21:57:26.250Z | 277.01° WNW | 34.607° | 2026-02-03 22:00:26.250Z | 218.273° SW |
| 6 mins | 2026-02-04 08:42:26.250Z | 173.344° S | 2026-02-04 08:45:26.250Z | 312.34° NW | 43.099° | 2026-02-04 08:48:26.250Z | 343.819° N |
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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