OBJECT E, 67678
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 E, 67678 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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67678 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 E
1 67678U 26023E 26037.83165436 .00006205 00000-0 27128-3 0 9997
2 67678 96.6374 114.3623 0018164 237.2347 122.7142 15.22227869 158Epoch: 2026-02-06T19:57Z
TLE epoch observation values (Epoch: 2026-02-06T19:57:34.936Z)
Latitude
0°
Longitude
38.00285°
Altitude
509.005 km
Speed
7.606 km/s
True Right ascension
07h 37m 26s
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
23:34:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.54 km
Perigee altitude
483.568 km
Semi-major axis
6,874.191 km
Eccentricity
0.00182
Inclination
96.6374°
RAAN
114.3623°
Arg. of periapsis
237.2347°
True anomaly
122.88911°
Mean anomaly
122.7142°
Eccentric anomaly
122.80168°
Mean motion
3.80812 °/min
Orbital period
94.53 mins
BSTAR
0.00027128
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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 E 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 | 2026-02-08 05:13:02.184Z | 177.884° S | 2026-02-08 05:16:02.184Z | 273.93° WNW | 42.84° | 2026-02-08 05:19:02.184Z | 342.57° N |
| 5 mins | 2026-02-08 18:17:02.184Z | 343.583° N | 2026-02-08 18:19:02.184Z | 292.121° WNW | 31.006° | 2026-02-08 18:22:02.184Z | 221.401° SW |
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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