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 25301.31345289 .00022354 00000-0 84958-3 0 9991
2 59777 97.6352 61.9442 0008595 248.5174 111.5148 15.26777214 80240Epoch: 2025-10-28T07:31Z
TLE epoch observation values (Epoch: 2025-10-28T07:31:22.329Z)
Latitude
-0.00004°
Longitude
-87.80157°
Altitude
490.715 km
Speed
7.618 km/s
True Right ascension
04h 07m 46s
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
04:11:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.317 km
Perigee altitude
476.524 km
Semi-major axis
6,860.558 km
Eccentricity
0.00086
Inclination
97.6352°
RAAN
61.9442°
Arg. of periapsis
248.5174°
True anomaly
111.60639°
Mean anomaly
111.5148°
Eccentric anomaly
111.5606°
Mean motion
3.81948 °/min
Orbital period
94.25 mins
BSTAR
0.00084958
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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 | 2025-10-29 08:49:02.691Z | 207.49° SW | 2025-10-29 08:52:02.691Z | 276.387° WNW | 24.534° | 2025-10-29 08:54:02.691Z | 316.883° NNW |
| 4 mins | 2025-10-29 21:51:02.691Z | 320.483° NNW | 2025-10-29 21:52:02.691Z | 297.644° NW | 20.378° | 2025-10-29 21:55:02.691Z | 239.279° WSW |
| 5 mins | 2025-10-30 08:25:02.691Z | 182.992° SSW | 2025-10-30 08:27:02.691Z | 228.906° WSW | 39.855° | 2025-10-30 08:30:02.691Z | 336.968° NNW |
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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