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: 5 hours ago
TLE from 5 hours ago
0 GNOMES-5
1 60574U 24149DL 26220.21584649 .00001592 00000-0 12751-3 0 9999
2 60574 97.7145 297.9545 0007025 333.4839 26.6025 15.01577548107962Epoch: 2026-08-08T05:10Z
TLE epoch observation values (Epoch: 2026-08-08T05:10:49.136Z)
Latitude
-0.00003°
Longitude
-96.48061°
Altitude
560.728 km
Speed
7.583 km/s
True Right ascension
19h 51m 49s
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
00:06:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.908 km
Perigee altitude
554.162 km
Semi-major axis
6,937.172 km
Eccentricity
0.0007
Inclination
97.7145°
RAAN
297.9545°
Arg. of periapsis
333.4839°
True anomaly
26.63858°
Mean anomaly
26.6025°
Eccentric anomaly
26.62054°
Mean motion
3.75638 °/min
Orbital period
95.84 mins
BSTAR
0.00012751
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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 | 2026-08-08 18:32:42.027Z | 352.592° N | 2026-08-08 18:35:42.027Z | 271.299° WNW | 34.72° | 2026-08-08 18:38:42.027Z | 216.595° SW |
| 6 mins | 2026-08-09 05:18:42.027Z | 168.862° S | 2026-08-09 05:20:42.027Z | 187.451° SSW | 44.576° | 2026-08-09 05:24:42.027Z | 346.893° N |
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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