OBJECT F, 59778
Orbit data source: Space-Track
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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT F, 59778 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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59778 intel report (Beta)
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OBJECT F 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 F
1 59778U 24092F 25260.07283431 .00014904 00000-0 59545-3 0 9995
2 59778 97.6297 19.9556 0009801 40.6349 319.5618 15.25190954 73966Epoch: 2025-09-17T01:44Z
TLE epoch observation values (Epoch: 2025-09-17T01:44:52.884Z)
Latitude
-0.00002°
Longitude
-2.51877°
Altitude
488.181 km
Speed
7.624 km/s
True Right ascension
01h 19m 49s
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
18:31:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.909 km
Perigee altitude
480.452 km
Semi-major axis
6,865.318 km
Eccentricity
0.00098
Inclination
97.6297°
RAAN
19.9556°
Arg. of periapsis
40.6349°
True anomaly
319.48888°
Mean anomaly
319.5618°
Eccentric anomaly
319.52535°
Mean motion
3.81551 °/min
Orbital period
94.35 mins
BSTAR
0.00059545
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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 F 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 | 2025-09-18 07:47:25.677Z | 147.837° SSE | 2025-09-18 07:50:25.677Z | 87.558° E | 36.061° | 2025-09-18 07:53:25.677Z | 2.956° NNE |
| 5 mins | 2025-09-18 20:50:25.677Z | 24.044° NE | 2025-09-18 20:52:25.677Z | 115.705° SE | 42.623° | 2025-09-18 20:55:25.677Z | 183.934° SSW |
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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