TIGER-8, 59120
Orbit data source: Space-Track
TIGER-8, 59120 is a payload satellite owned by OQ Tech (RW) 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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59120 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
RW / RWARelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 TIGER-8
1 59120U 24043Y 25336.27748197 .00013501 00000-0 33876-3 0 9994
2 59120 97.5303 113.1240 0008299 184.7301 175.3868 15.40112111 97438Epoch: 2025-12-02T06:39Z
TLE epoch observation values (Epoch: 2025-12-02T06:39:34.442Z)
Latitude
0.00003°
Longitude
-58.13445°
Altitude
454.538 km
Speed
7.637 km/s
True Right ascension
07h 32m 29s
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
10:16:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.383 km
Perigee altitude
437.062 km
Semi-major axis
6,820.86 km
Eccentricity
0.00083
Inclination
97.5303°
RAAN
113.124°
Arg. of periapsis
184.7301°
True anomaly
175.39444°
Mean anomaly
175.3868°
Eccentric anomaly
175.39062°
Mean motion
3.85287 °/min
Orbital period
93.44 mins
BSTAR
0.00033876
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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.TIGER-8 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-03 09:18:44.692Z | 164.089° S | 2025-12-03 09:20:44.692Z | 13.879° NNE | 44.442° | 2025-12-03 09:23:44.692Z | 349.198° 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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