OBJECT G, 67369
Orbit data source: Space-Track
OBJECT G, 67369 is a satellite in SSO that was launched on Sun, 11 Jan 2026 UTC via an FALCON 9 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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67369 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Penn State University (US)Manufacturer
NanoAvionics US
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
11.4 kg wet, 11.4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 OBJECT G
1 67369U 26004G 26093.55612708 .00004712 00000-0 52595-3 0 9990
2 67369 97.7985 93.2717 0008259 40.9819 319.2017 14.87453259 12196Epoch: 2026-04-03T13:20Z
TLE epoch observation values (Epoch: 2026-04-03T13:20:49.379Z)
Latitude
0°
Longitude
61.17739°
Altitude
604.565 km
Speed
7.56 km/s
True Right ascension
06h 13m 05s
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
03:52:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.688 km
Perigee altitude
597.157 km
Semi-major axis
6,981.059 km
Eccentricity
0.00083
Inclination
97.7985°
RAAN
93.2717°
Arg. of periapsis
40.9819°
True anomaly
319.13981°
Mean anomaly
319.2017°
Eccentric anomaly
319.17076°
Mean motion
3.72101 °/min
Orbital period
96.75 mins
BSTAR
0.00052595
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Other satellites on launch #4 in the year 2026 (2026-01-11 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 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 | 2026-04-03 23:10:53.676Z | 118.718° SE | 2026-04-03 23:13:53.676Z | 60.524° ENE | 23.847° | 2026-04-03 23:16:53.676Z | 13.589° NNE |
| 4 mins | 2026-04-04 00:47:53.676Z | 235.106° WSW | 2026-04-04 00:48:53.676Z | 255.304° W | 21.699° | 2026-04-04 00:51:53.676Z | 311.157° NW |
| 6 mins | 2026-04-04 12:31:53.676Z | 27.407° NE | 2026-04-04 12:34:53.676Z | 114.367° SE | 39.282° | 2026-04-04 12:37:53.676Z | 175.547° S |
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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