OBJECT G, 67680
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT G, 67680 is a satellite owned by VVKO VKS (CIS) in SSO that was launched on Thu, 05 Feb 2026 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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67680 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown (RU)
Mission
Spacecraft
Bus & Motor
UNK, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OBJECT G
1 67680U 26023G 26037.83150302 .00006474 00000-0 28118-3 0 9994
2 67680 96.6428 116.8488 0021860 225.7092 134.2354 15.22375887 149Epoch: 2026-02-06T19:57Z
TLE epoch observation values (Epoch: 2026-02-06T19:57:21.860Z)
Latitude
-0.00006°
Longitude
40.54399°
Altitude
512.297 km
Speed
7.602 km/s
True Right ascension
07h 47m 23s
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
23:34:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.634 km
Perigee altitude
480.582 km
Semi-major axis
6,873.745 km
Eccentricity
0.00219
Inclination
96.6428°
RAAN
116.8488°
Arg. of periapsis
225.7092°
True anomaly
134.41453°
Mean anomaly
134.2354°
Eccentric anomaly
134.325°
Mean motion
3.80849 °/min
Orbital period
94.53 mins
BSTAR
0.00028118
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Other satellites on launch #23 in the year 2026 (2026-02-05 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-08 05:11:56.402Z | 166.569° S | 2026-02-08 05:15:56.402Z | 1.728° NNE | 43.847° | 2026-02-08 05:18:56.402Z | 350.1° N |
| 5 mins | 2026-02-08 18:16:56.402Z | 349.983° N | 2026-02-08 18:18:56.402Z | 277.597° WNW | 37.806° | 2026-02-08 18:21:56.402Z | 209.826° SW |
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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