OBJECT Z, 61758
Orbit data source: Space-Track
OBJECT Z, 61758 is a payload satellite in SSO that was launched on Mon, 04 Nov 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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61758 intel report (Beta)
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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
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OBJECT Z
1 61758U 24199Z 26309.95735501 .00002576 00000-0 21964-3 0 9992
2 61758 97.3147 140.7697 0004509 326.8461 33.2480 14.98533409156369Epoch: 2026-11-05T22:58Z
TLE epoch observation values (Epoch: 2026-11-05T22:58:35.472Z)
Latitude
-0°
Longitude
110.93804°
Altitude
571.87 km
Speed
7.576 km/s
True Right ascension
09h 23m 04s
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
09:28:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.55 km
Perigee altitude
565.285 km
Semi-major axis
6,946.555 km
Eccentricity
0.00045
Inclination
97.3147°
RAAN
140.7697°
Arg. of periapsis
326.8461°
True anomaly
33.27634°
Mean anomaly
33.248°
Eccentric anomaly
33.26217°
Mean motion
3.74877 °/min
Orbital period
96.03 mins
BSTAR
0.00021964
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Other satellites on launch #199 in the year 2024 (2024-11-04 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 Z 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 | 2026-11-06 13:31:33.633Z | 205.613° SW | 2026-11-06 13:34:33.633Z | 269.112° W | 31.995° | 2026-11-06 13:37:33.633Z | 324.279° NNW |
| 5 mins | 2026-11-07 01:12:33.633Z | 44.954° NE | 2026-11-07 01:14:33.633Z | 94.081° ESE | 35.647° | 2026-11-07 01:17:33.633Z | 158.555° S |
| 4 mins | 2026-11-07 12:00:33.633Z | 90.56° ESE | 2026-11-07 12:01:33.633Z | 70.944° E | 19.995° | 2026-11-07 12:04:33.633Z | 22.112° NNE |
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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