GNOMES-5, 60574
Orbit data source: Space-Track
GNOMES-5, 60574 is a payload satellite owned by PlanetiQ (US) in SSO that was launched on Fri, 16 Aug 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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60574 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Canyon
Mission
Operational Commercial Communications
Bus & Motor
XSAT, Unknown motor
Mass
~41 kg wet, ~41 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.162 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GNOMES-5
1 60574U 24149DL 26170.76501404 .00003784 00000-0 29921-3 0 9993
2 60574 97.7096 248.8287 0008373 112.1920 248.0193 15.01224765100548Epoch: 2026-06-19T18:21Z
TLE epoch observation values (Epoch: 2026-06-19T18:21:37.213Z)
Latitude
-0.00002°
Longitude
65.43435°
Altitude
568.355 km
Speed
7.576 km/s
True Right ascension
16h 35m 18s
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
07:20:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.932 km
Perigee altitude
554.313 km
Semi-major axis
6,938.26 km
Eccentricity
0.00084
Inclination
97.7096°
RAAN
248.8287°
Arg. of periapsis
112.192°
True anomaly
247.93036°
Mean anomaly
248.0193°
Eccentric anomaly
247.97483°
Mean motion
3.7555 °/min
Orbital period
95.86 mins
BSTAR
0.00029921
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.GNOMES-5 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 04:07:07.919Z | 96.052° ESE | 2026-06-21 04:09:07.919Z | 64.676° ENE | 13.962° | 2026-06-21 04:11:07.919Z | 33.85° NE |
| 6 mins | 2026-06-21 05:41:07.919Z | 197.438° SSW | 2026-06-21 05:44:07.919Z | 280.351° WNW | 32.946° | 2026-06-21 05:47:07.919Z | 331.478° NNW |
| 4 mins | 2026-06-21 17:21:07.919Z | 63.154° ENE | 2026-06-21 17:22:07.919Z | 83.828° E | 21.343° | 2026-06-21 17:25:07.919Z | 142.719° SSE |
| 4 mins | 2026-06-21 18:56:07.919Z | 321.281° NNW | 2026-06-21 18:57:07.919Z | 299.886° NW | 21.827° | 2026-06-21 19:00:07.919Z | 242.232° WSW |
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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