ANTELSAT, 40034
Orbit data source: Space-Track
ANTELSAT, 40034 is an Uruguayan payload satellite in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40034 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UY / URYRelated business
Manufacturer
UdelaR FING
Mission
Non-operational Civil Tech/Com
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
~2 kg wet, ~2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Ant, 0.1 m
Radar Cross Section
0.040 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ANTELSAT
1 40034U 14033AA 26032.98511217 .00005465 00000-0 56493-3 0 9999
2 40034 97.7574 190.9965 0044973 143.0579 217.3751 14.89764563625672Epoch: 2026-02-01T23:38Z
TLE epoch observation values (Epoch: 2026-02-01T23:38:33.691Z)
Latitude
0.00001°
Longitude
64.16922°
Altitude
626.701 km
Speed
7.532 km/s
True Right ascension
12h 43m 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
16:06:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.055 km
Perigee altitude
564.329 km
Semi-major axis
6,973.829 km
Eccentricity
0.0045
Inclination
97.7574°
RAAN
190.9965°
Arg. of periapsis
143.0579°
True anomaly
217.06366°
Mean anomaly
217.3751°
Eccentric anomaly
217.21924°
Mean motion
3.7268 °/min
Orbital period
96.6 mins
BSTAR
0.00056493
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Other satellites on launch #33 in the year 2014 (2014-06-19 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ANTELSAT 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 | 2026-02-02 22:47:31.320Z | 36.776° NE | 2026-02-02 22:50:31.320Z | 105.324° ESE | 30.409° | 2026-02-02 22:53:31.320Z | 162.544° S |
| 5 mins | 2026-02-03 09:39:31.320Z | 104.983° ESE | 2026-02-03 09:41:31.320Z | 62.463° ENE | 23° | 2026-02-03 09:44:31.320Z | 15.09° NNE |
| 5 mins | 2026-02-03 11:14:31.320Z | 219.912° SW | 2026-02-03 11:16:31.320Z | 256.828° W | 23.002° | 2026-02-03 11:19:31.320Z | 313.267° NW |
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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