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: 22 hours ago
TLE from 22 hours ago
0 GNOMES-5
1 60574U 24149DL 26297.17411231 .00003882 00000-0 30097-3 0 9991
2 60574 97.7004 14.3634 0008005 85.1452 275.0687 15.01958450119510Epoch: 2026-10-24T04:10Z
TLE epoch observation values (Epoch: 2026-10-24T04:10:43.303Z)
Latitude
0.00004°
Longitude
-80.90113°
Altitude
563.429 km
Speed
7.58 km/s
True Right ascension
00h 57m 27s
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
21:31:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.413 km
Perigee altitude
552.308 km
Semi-major axis
6,935.997 km
Eccentricity
0.0008
Inclination
97.7004°
RAAN
14.3634°
Arg. of periapsis
85.1452°
True anomaly
274.97732°
Mean anomaly
275.0687°
Eccentric anomaly
275.02301°
Mean motion
3.75733 °/min
Orbital period
95.81 mins
BSTAR
0.00030097
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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 | 2026-10-25 04:18:57.033Z | 106.836° ESE | 2026-10-25 04:20:57.033Z | 75.386° E | 17.443° | 2026-10-25 04:23:57.033Z | 25.809° NE |
| 5 mins | 2026-10-25 05:53:57.033Z | 211.391° SW | 2026-10-25 05:55:57.033Z | 259.165° W | 33.176° | 2026-10-25 05:58:57.033Z | 322.53° NNW |
| 5 mins | 2026-10-25 17:32:57.033Z | 54.377° ENE | 2026-10-25 17:34:57.033Z | 103.845° ESE | 29.304° | 2026-10-25 17:37:57.033Z | 156.594° SSE |
| 4 mins | 2026-10-25 19:07:57.033Z | 320.812° NNW | 2026-10-25 19:08:57.033Z | 302.348° NW | 19.334° | 2026-10-25 19:11:57.033Z | 249.391° W |
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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