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: 9 hours ago
TLE from 9 hours ago
0 ANTELSAT
1 40034U 14033AA 26078.98605740 .00003568 00000-0 36728-3 0 9995
2 40034 97.7656 236.1722 0043390 353.4919 6.5730 14.90231865632527Epoch: 2026-03-19T23:39Z
TLE epoch observation values (Epoch: 2026-03-19T23:39:55.359Z)
Latitude
0.00001°
Longitude
63.66392°
Altitude
570.18 km
Speed
7.592 km/s
True Right ascension
15h 44m 41s
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
13:18:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.486 km
Perigee altitude
563.98 km
Semi-major axis
6,972.37 km
Eccentricity
0.00434
Inclination
97.7656°
RAAN
236.1722°
Arg. of periapsis
353.4919°
True anomaly
6.63022°
Mean anomaly
6.573°
Eccentric anomaly
6.60158°
Mean motion
3.72797 °/min
Orbital period
96.57 mins
BSTAR
0.00036728
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-20 09:28:53.425Z | 112.634° SE | 2026-03-20 09:31:53.425Z | 63.07° ENE | 18.625° | 2026-03-20 09:33:53.425Z | 29.053° NE |
| 5 mins | 2026-03-20 11:04:53.425Z | 213.227° SW | 2026-03-20 11:06:53.425Z | 256.012° W | 26.823° | 2026-03-20 11:09:53.425Z | 318.842° NNW |
| 6 mins | 2026-03-20 22:48:53.425Z | 40.404° NE | 2026-03-20 22:50:53.425Z | 84.263° E | 32.405° | 2026-03-20 22:54:53.425Z | 166.358° S |
| 4 mins | 2026-03-21 00:24:53.425Z | 321.883° NNW | 2026-03-21 00:26:53.425Z | 288.649° WNW | 16.833° | 2026-03-21 00:28:53.425Z | 258.242° W |
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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