COSMOS 2604, 67678
Orbit data source: Space-Track
COSMOS 2604, 67678 is a payload 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). 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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67678 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown (RU)
Mission
Operational Defense Imaging
Bus & Motor
UNK, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 0.5 m
Radar Cross Section
3.727 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 COSMOS 2604
1 67678U 26023E 26170.92963279 .00009693 00000-0 38397-3 0 9990
2 67678 96.6204 232.0628 0019665 121.2625 239.0545 15.25403467 20425Epoch: 2026-06-19T22:18Z
TLE epoch observation values (Epoch: 2026-06-19T22:18:40.273Z)
Latitude
0.00004°
Longitude
-10.75656°
Altitude
499.659 km
Speed
7.611 km/s
True Right ascension
15h 28m 15s
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
08:42:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500 km
Perigee altitude
473.002 km
Semi-major axis
6,864.638 km
Eccentricity
0.00197
Inclination
96.6204°
RAAN
232.0628°
Arg. of periapsis
121.2625°
True anomaly
238.86148°
Mean anomaly
239.0545°
Eccentric anomaly
238.95796°
Mean motion
3.81607 °/min
Orbital period
94.34 mins
BSTAR
0.00038397
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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 2604 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 | 2026-06-21 04:21:09.366Z | 180.453° SSW | 2026-06-21 04:24:09.366Z | 287.464° WNW | 41.122° | 2026-06-21 04:27:09.366Z | 341.866° N |
| 5 mins | 2026-06-21 17:23:09.366Z | 344.48° N | 2026-06-21 17:25:09.366Z | 295.236° NW | 30.039° | 2026-06-21 17:28:09.366Z | 221.968° 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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