COSMOS 2600, 67674
Orbit data source: Space-Track
COSMOS 2600, 67674 is a payload satellite owned by MO RF (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). 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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67674 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Operational spacecraft
Bus & Motor
EMKA, Unknown motor
Mass
520 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 COSMOS 2600
1 67674U 26023A 26071.93810518 .00079942 00000-0 36884-3 0 9997
2 67674 96.6421 147.4784 0001980 68.7083 291.4400 15.83329859 5564Epoch: 2026-03-12T22:30Z
TLE epoch observation values (Epoch: 2026-03-12T22:30:52.287Z)
Latitude
0.00001°
Longitude
-0.82028°
Altitude
323.744 km
Speed
7.714 km/s
True Right ascension
09h 49m 54s
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
12:18:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
319.207 km
Perigee altitude
316.556 km
Semi-major axis
6,696.019 km
Eccentricity
0.0002
Inclination
96.6421°
RAAN
147.4784°
Arg. of periapsis
68.7083°
True anomaly
291.41888°
Mean anomaly
291.44°
Eccentric anomaly
291.42944°
Mean motion
3.96112 °/min
Orbital period
90.88 mins
BSTAR
0.00036884
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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.COSMOS 2600 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. |
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| COSMOS 2600 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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