OBJECT E, 59777
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, 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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Edit Public Description
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, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OBJECT E
1 59777U 24092E 25315.27042339 .00027732 00000-0 10317-2 0 9993
2 59777 97.6366 76.2231 0008913 197.2482 162.8455 15.27435531 82376Epoch: 2025-11-11T06:29Z
TLE epoch observation values (Epoch: 2025-11-11T06:29:24.580Z)
Latitude
-0.00004°
Longitude
-71.7887°
Altitude
492.421 km
Speed
7.615 km/s
True Right ascension
05h 04m 53s
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
05:44:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.561 km
Perigee altitude
474.335 km
Semi-major axis
6,858.585 km
Eccentricity
0.00089
Inclination
97.6366°
RAAN
76.2231°
Arg. of periapsis
197.2482°
True anomaly
162.87559°
Mean anomaly
162.8455°
Eccentric anomaly
162.86055°
Mean motion
3.82113 °/min
Orbital period
94.21 mins
BSTAR
0.0010317
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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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-12 20:48:24.401Z | 36.643° NE | 2025-11-12 20:50:24.401Z | 113.784° SE | 36.258° | 2025-11-12 20:53:24.401Z | 174.793° S |
| 4 mins | 2025-11-13 08:56:24.401Z | 220.782° SW | 2025-11-13 08:58:24.401Z | 267.719° W | 22.524° | 2025-11-13 09:00:24.401Z | 310.739° NW |
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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