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: 18 hours ago
TLE from 18 hours ago
0 GNOMES-5
1 60574U 24149DL 26080.22465126 .00004627 00000-0 37278-3 0 9995
2 60574 97.6860 159.1631 0008170 59.2582 300.9445 15.00385180 86968Epoch: 2026-03-21T05:23Z
TLE epoch observation values (Epoch: 2026-03-21T05:23:29.868Z)
Latitude
-0.00008°
Longitude
-100.45977°
Altitude
565.849 km
Speed
7.58 km/s
True Right ascension
10h 36m 39s
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
04:24:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.382 km
Perigee altitude
557.041 km
Semi-major axis
6,940.849 km
Eccentricity
0.00082
Inclination
97.686°
RAAN
159.1631°
Arg. of periapsis
59.2582°
True anomaly
300.86416°
Mean anomaly
300.9445°
Eccentric anomaly
300.90434°
Mean motion
3.7534 °/min
Orbital period
95.91 mins
BSTAR
0.00037278
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-22 05:32:27.512Z | 193.174° SSW | 2026-03-22 05:34:27.512Z | 254.094° W | 38.39° | 2026-03-22 05:37:27.512Z | 333.176° NNW |
| 4 mins | 2026-03-22 17:12:27.512Z | 67.026° ENE | 2026-03-22 17:13:27.512Z | 86.046° E | 18.644° | 2026-03-22 17:16:27.512Z | 138.647° SSE |
| 5 mins | 2026-03-22 18:46:27.512Z | 339.929° N | 2026-03-22 18:48:27.512Z | 301.609° NW | 25.16° | 2026-03-22 18:51:27.512Z | 237.503° 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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