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: 6 hours ago
TLE from 6 hours ago
0 GNOMES-5
1 60574U 24149DL 26126.16746149 .00004643 00000-0 36983-3 0 9996
2 60574 97.6947 204.6114 0006112 268.4459 91.6065 15.00836954 93855Epoch: 2026-05-06T04:01Z
TLE epoch observation values (Epoch: 2026-05-06T04:01:08.672Z)
Latitude
-0.00002°
Longitude
-79.70657°
Altitude
567.492 km
Speed
7.577 km/s
True Right ascension
13h 38m 26s
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
17:31:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.559 km
Perigee altitude
557.077 km
Semi-major axis
6,939.455 km
Eccentricity
0.00061
Inclination
97.6947°
RAAN
204.6114°
Arg. of periapsis
268.4459°
True anomaly
91.67651°
Mean anomaly
91.6065°
Eccentric anomaly
91.6415°
Mean motion
3.75453 °/min
Orbital period
95.88 mins
BSTAR
0.00036983
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-06 17:23:55.273Z | 41.861° NE | 2026-05-06 17:26:55.273Z | 99.714° ESE | 24.679° | 2026-05-06 17:29:55.273Z | 153.084° SSE |
| 4 mins | 2026-05-06 18:59:55.273Z | 325.197° NNW | 2026-05-06 19:01:55.273Z | 285.369° WNW | 19.943° | 2026-05-06 19:03:55.273Z | 250.08° W |
| 5 mins | 2026-05-07 05:45:55.273Z | 212.813° SW | 2026-05-07 05:47:55.273Z | 270.548° WNW | 30.775° | 2026-05-07 05:50:55.273Z | 327.192° NNW |
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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