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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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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TIGER-8
1 59120U 24043Y 26234.85356804 .00008118 00000-0 16975-3 0 9995
2 59120 97.5616 26.1948 0006250 333.6068 26.4861 15.45745957138084Epoch: 2026-08-22T20:29Z
TLE epoch observation values (Epoch: 2026-08-22T20:29:08.278Z)
Latitude
-0.00007°
Longitude
107.7523°
Altitude
428.499 km
Speed
7.657 km/s
True Right ascension
01h 44m 46s
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
15:55:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
430.378 km
Perigee altitude
421.873 km
Semi-major axis
6,804.263 km
Eccentricity
0.00063
Inclination
97.5616°
RAAN
26.1948°
Arg. of periapsis
333.6068°
True anomaly
26.51806°
Mean anomaly
26.4861°
Eccentric anomaly
26.50208°
Mean motion
3.86698 °/min
Orbital period
93.1 mins
BSTAR
0.00016975
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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 | 2026-08-24 09:54:49.610Z | 142.085° SSE | 2026-08-24 09:56:49.610Z | 86.408° E | 35.033° | 2026-08-24 09:59:49.610Z | 2.259° NNE |
| 4 mins | 2026-08-24 22:46:49.610Z | 38.073° NE | 2026-08-24 22:48:49.610Z | 123.232° SE | 34.474° | 2026-08-24 22:50:49.610Z | 169.967° S |
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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