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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OBJECT E radio frequencies
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Sputniks
Mission
Operational spacecraft
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
Unknown
Radar Cross Section
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 25260.91581718 .00012708 00000-0 51363-3 0 9996
2 59777 97.6303 20.7129 0009620 37.2382 322.9520 15.24841793 74084Epoch: 2025-09-17T21:58Z
TLE epoch observation values (Epoch: 2025-09-17T21:58:46.604Z)
Latitude
-0.00006°
Longitude
53.93381°
Altitude
489.078 km
Speed
7.623 km/s
True Right ascension
01h 22m 51s
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
16:37:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.835 km
Perigee altitude
481.624 km
Semi-major axis
6,866.367 km
Eccentricity
0.00096
Inclination
97.6303°
RAAN
20.7129°
Arg. of periapsis
37.2382°
True anomaly
322.88552°
Mean anomaly
322.952°
Eccentric anomaly
322.91877°
Mean motion
3.81463 °/min
Orbital period
94.37 mins
BSTAR
0.00051363
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-19 07:12:30.402Z | 105.848° ESE | 2025-09-19 07:14:30.402Z | 68.771° E | 16.5° | 2025-09-19 07:16:30.402Z | 31.333° NE |
| 4 mins | 2025-09-19 08:46:30.402Z | 227.158° WSW | 2025-09-19 08:47:30.402Z | 252.139° W | 23.421° | 2025-09-19 08:50:30.402Z | 318.094° NNW |
| 4 mins | 2025-09-19 20:14:30.402Z | 60.317° ENE | 2025-09-19 20:16:30.402Z | 106.859° ESE | 20.335° | 2025-09-19 20:18:30.402Z | 143.893° SSE |
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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