OBJECT G, 60209
Orbit data source: Space-Track
OBJECT G, 60209 is an American satellite in SSO that was launched on Thu, 04 Jul 2024 UTC via an FIREFLY ALPHA launch vehicle from the Air Force Western Test Range (AFWTR). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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60209 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
UME
Mission
Operational Amateur Science
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 OBJECT G
1 60209U 24125G 26306.07174194 .00221817 19779-4 75675-3 0 9992
2 60209 97.1969 168.5596 0006351 69.2252 290.9702 15.89741193131249Epoch: 2026-11-02T01:43Z
TLE epoch observation values (Epoch: 2026-11-02T01:43:18.503Z)
Latitude
0.00005°
Longitude
101.37848°
Altitude
304.682 km
Speed
7.726 km/s
True Right ascension
11h 14m 14s
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
09:38:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
304.114 km
Perigee altitude
295.631 km
Semi-major axis
6,678.009 km
Eccentricity
0.00064
Inclination
97.1969°
RAAN
168.5596°
Arg. of periapsis
69.2252°
True anomaly
290.90222°
Mean anomaly
290.9702°
Eccentric anomaly
290.93621°
Mean motion
3.97716 °/min
Orbital period
90.52 mins
BSTAR
0.00075675
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Other satellites on launch #125 in the year 2024 (2024-07-04 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.OBJECT G Visibility
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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. |
|---|---|---|---|---|---|---|---|
| OBJECT G is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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