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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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: 1 day ago
TLE from 1 day ago
0 ANTELSAT
1 40034U 14033AA 26191.22034880 .00001597 00000-0 16451-3 0 9990
2 40034 97.7797 346.6585 0042488 341.9376 18.0330 14.91041847649244Epoch: 2026-07-10T05:17Z
TLE epoch observation values (Epoch: 2026-07-10T05:17:18.136Z)
Latitude
-0.00005°
Longitude
-20.81811°
Altitude
569.561 km
Speed
7.591 km/s
True Right ascension
23h 06m 38s
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
03:05:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.32 km
Perigee altitude
562.093 km
Semi-major axis
6,969.843 km
Eccentricity
0.00425
Inclination
97.7797°
RAAN
346.6585°
Arg. of periapsis
341.9376°
True anomaly
18.18448°
Mean anomaly
18.033°
Eccentric anomaly
18.10867°
Mean motion
3.73 °/min
Orbital period
96.51 mins
BSTAR
0.00016451
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-11 22:09:26.060Z | 66.146° ENE | 2026-07-11 22:11:26.060Z | 96.862° ESE | 14.595° | 2026-07-11 22:13:26.060Z | 125.44° SE |
| 6 mins | 2026-07-11 23:44:26.060Z | 349.432° N | 2026-07-11 23:47:26.060Z | 266.755° W | 34.206° | 2026-07-11 23:50:26.060Z | 218.055° SW |
| 6 mins | 2026-07-12 10:34:26.060Z | 177.72° S | 2026-07-12 10:36:26.060Z | 209.67° SW | 41.583° | 2026-07-12 10:40:26.060Z | 342.042° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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