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: 2 days ago
TLE from 2 days ago
0 ANTELSAT
1 40034U 14033AA 26171.35555153 .00002382 00000-0 24280-3 0 9995
2 40034 97.7784 327.0821 0044124 47.4977 312.9955 14.90924840646282Epoch: 2026-06-20T08:31Z
TLE epoch observation values (Epoch: 2026-06-20T08:31:59.652Z)
Latitude
-0.00006°
Longitude
-69.4878°
Altitude
577.177 km
Speed
7.583 km/s
True Right ascension
21h 48m 19s
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
21:40:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
622.827 km
Perigee altitude
561.316 km
Semi-major axis
6,970.208 km
Eccentricity
0.00441
Inclination
97.7784°
RAAN
327.0821°
Arg. of periapsis
47.4977°
True anomaly
312.62429°
Mean anomaly
312.9955°
Eccentric anomaly
312.81003°
Mean motion
3.72971 °/min
Orbital period
96.52 mins
BSTAR
0.0002428
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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 | 2026-06-22 22:20:35.559Z | 66.443° ENE | 2026-06-22 22:22:35.559Z | 102.988° ESE | 17.887° | 2026-06-22 22:24:35.559Z | 134.159° SE |
| 5 mins | 2026-06-22 23:55:35.559Z | 339.026° N | 2026-06-22 23:57:35.559Z | 295.02° NW | 28.543° | 2026-06-23 00:00:35.559Z | 232.28° WSW |
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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