CONNECTA IOT-5, 62703
Orbit data source: Space-Track
CONNECTA IOT-5, 62703 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62703 intel report (Beta)
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Identifier
Orbit
Country
TR / TURKRelated business
Manufacturer
Plan-S
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 2.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CONNECTA IOT-5
1 62703U 25009CY 26080.16409685 .00001481 00000-0 14233-3 0 9999
2 62703 97.7057 160.4090 0002443 31.4554 328.6812 14.94526310 64229Epoch: 2026-03-21T03:56Z
TLE epoch observation values (Epoch: 2026-03-21T03:56:17.967Z)
Latitude
-0.00006°
Longitude
-77.3546°
Altitude
585.437 km
Speed
7.568 km/s
True Right ascension
10h 41m 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
17:24:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.556 km
Perigee altitude
579.156 km
Semi-major axis
6,958.993 km
Eccentricity
0.00024
Inclination
97.7057°
RAAN
160.409°
Arg. of periapsis
31.4554°
True anomaly
328.66664°
Mean anomaly
328.6812°
Eccentric anomaly
328.67392°
Mean motion
3.73873 °/min
Orbital period
96.29 mins
BSTAR
0.00014233
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.CONNECTA IOT-5 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 | 2026-03-22 17:28:32.927Z | 41.44° NE | 2026-03-22 17:31:32.927Z | 98.394° ESE | 25.312° | 2026-03-22 17:34:32.927Z | 152.647° SSE |
| 4 mins | 2026-03-22 19:05:32.927Z | 315.554° NNW | 2026-03-22 19:06:32.927Z | 295.152° NW | 20.367° | 2026-03-22 19:09:32.927Z | 244.237° WSW |
| 5 mins | 2026-03-23 05:53:32.927Z | 213.433° SW | 2026-03-23 05:55:32.927Z | 264.016° W | 29.437° | 2026-03-23 05:58:32.927Z | 323.755° NNW |
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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