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, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 TIGER-8
1 59120U 24043Y 26083.89710580 .00010568 00000-0 24131-3 0 9991
2 59120 97.5424 229.3629 0008941 142.3271 217.8604 15.43021115114787Epoch: 2026-03-24T21:31Z
TLE epoch observation values (Epoch: 2026-03-24T21:31:49.941Z)
Latitude
0.00001°
Longitude
84.03664°
Altitude
445.13 km
Speed
7.642 km/s
True Right ascension
15h 17m 27s
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
13:51:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
440.231 km
Perigee altitude
428.049 km
Semi-major axis
6,812.277 km
Eccentricity
0.00089
Inclination
97.5424°
RAAN
229.3629°
Arg. of periapsis
142.3271°
True anomaly
217.79757°
Mean anomaly
217.8604°
Eccentric anomaly
217.82898°
Mean motion
3.86015 °/min
Orbital period
93.26 mins
BSTAR
0.00024131
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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 | 2026-03-25 10:06:10.497Z | 194.176° SSW | 2026-03-25 10:09:10.497Z | 264.622° W | 29.965° | 2026-03-25 10:11:10.497Z | 320.437° NNW |
| 5 mins | 2026-03-25 22:59:10.497Z | 349.969° N | 2026-03-25 23:02:10.497Z | 271.118° WNW | 27.917° | 2026-03-25 23:04:10.497Z | 226.394° WSW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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