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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Edit Public Description
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: 19 hours ago
TLE from 19 hours ago
0 GNOMES-5
1 60574U 24149DL 25287.20622285 .00006021 00000-0 50854-3 0 9997
2 60574 97.7067 2.9568 0003018 173.7552 186.3708 14.98467584 63280Epoch: 2025-10-14T04:56Z
TLE epoch observation values (Epoch: 2025-10-14T04:56:57.654Z)
Latitude
-0.00008°
Longitude
-94.28139°
Altitude
576.768 km
Speed
7.571 km/s
True Right ascension
00h 11m 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
18:56:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.735 km
Perigee altitude
566.542 km
Semi-major axis
6,946.775 km
Eccentricity
0.0003
Inclination
97.7067°
RAAN
2.9568°
Arg. of periapsis
173.7552°
True anomaly
186.36696°
Mean anomaly
186.3708°
Eccentric anomaly
186.36888°
Mean motion
3.74859 °/min
Orbital period
96.04 mins
BSTAR
0.00050854
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-15 05:06:37.583Z | 162.483° S | 2025-10-15 05:10:37.583Z | 9.491° NNE | 42.498° | 2025-10-15 05:13:37.583Z | 350.419° N |
| 5 mins | 2025-10-15 18:23:37.583Z | 349.971° N | 2025-10-15 18:25:37.583Z | 284.712° WNW | 38.094° | 2025-10-15 18:28:37.583Z | 213.836° SW |
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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