OBJECT E, 59777
Orbit data source: Space-Track
OBJECT E, 59777 is a satellite owned by Sitronics (CIS) in SSO that was launched on Thu, 16 May 2024 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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59777 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Sputniks
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 OBJECT E
1 59777U 24092E 26233.29930921 .00019665 00000-0 50998-3 0 9994
2 59777 97.6645 9.1565 0005435 275.3206 84.7419 15.39038742125757Epoch: 2026-08-21T07:11Z
TLE epoch observation values (Epoch: 2026-08-21T07:11:00.315Z)
Latitude
0.00001°
Longitude
-68.22088°
Altitude
451.721 km
Speed
7.642 km/s
True Right ascension
00h 36m 37s
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
19:02:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.611 km
Perigee altitude
442.194 km
Semi-major axis
6,824.039 km
Eccentricity
0.00054
Inclination
97.6645°
RAAN
9.1565°
Arg. of periapsis
275.3206°
True anomaly
84.80392°
Mean anomaly
84.7419°
Eccentric anomaly
84.77291°
Mean motion
3.85018 °/min
Orbital period
93.5 mins
BSTAR
0.00050998
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Other satellites on launch #92 in the year 2024 (2024-05-16 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
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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. |
|---|---|---|---|---|---|---|---|
| OBJECT E 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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