OBJECT T, 59068
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 T, 59068 is a satellite in LEO that was launched on Thu, 29 Feb 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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59068 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated 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: 13 hours ago
TLE from 13 hours ago
0 OBJECT T
1 59068U 24039T 25272.31409222 .00014464 00000-0 11876-2 0 9991
2 59068 95.3885 56.2483 0152971 157.3869 203.4193 14.90453098 85839Epoch: 2025-09-29T07:32Z
TLE epoch observation values (Epoch: 2025-09-29T07:32:17.567Z)
Latitude
0.00002°
Longitude
-65.14449°
Altitude
697.8 km
Speed
7.454 km/s
True Right ascension
03h 44m 59s
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
14:03:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
700.097 km
Perigee altitude
486.807 km
Semi-major axis
6,971.589 km
Eccentricity
0.0153
Inclination
95.3885°
RAAN
56.2483°
Arg. of periapsis
157.3869°
True anomaly
202.73463°
Mean anomaly
203.4193°
Eccentric anomaly
203.07577°
Mean motion
3.7286 °/min
Orbital period
96.55 mins
BSTAR
0.0011876
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Other satellites on launch #39 in the year 2024 (2024-02-29 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 T 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 | 2025-09-29 22:36:39.297Z | 1.842° NNE | 2025-09-29 22:39:39.297Z | 293.21° NW | 41.95° | 2025-09-29 22:42:39.297Z | 201.683° SSW |
| 6 mins | 2025-09-30 09:27:39.297Z | 143.191° SSE | 2025-09-30 09:30:39.297Z | 61.623° ENE | 36.931° | 2025-09-30 09:33:39.297Z | 5.791° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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