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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 12 hours ago
TLE from 12 hours ago
0 CONNECTA IOT-5
1 62703U 25009CY 26034.16569222 .00002008 00000-0 19176-3 0 9999
2 62703 97.7128 115.2304 0003490 127.2486 232.9053 14.94380308 57350Epoch: 2026-02-03T03:58Z
TLE epoch observation values (Epoch: 2026-02-03T03:58:35.807Z)
Latitude
-0.00005°
Longitude
-77.76932°
Altitude
588.81 km
Speed
7.565 km/s
True Right ascension
07h 40m 55s
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
18:04:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.739 km
Perigee altitude
578.881 km
Semi-major axis
6,959.447 km
Eccentricity
0.00035
Inclination
97.7128°
RAAN
115.2304°
Arg. of periapsis
127.2486°
True anomaly
232.87341°
Mean anomaly
232.9053°
Eccentric anomaly
232.88935°
Mean motion
3.73836 °/min
Orbital period
96.3 mins
BSTAR
0.00019176
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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 | 2026-02-03 17:24:28.839Z | 40.709° NE | 2026-02-03 17:27:28.839Z | 90.129° ESE | 22.913° | 2026-02-03 17:30:28.839Z | 146.251° SSE |
| 4 mins | 2026-02-03 19:01:28.839Z | 323.327° NNW | 2026-02-03 19:03:28.839Z | 279.835° WNW | 21.812° | 2026-02-03 19:05:28.839Z | 245.118° WSW |
| 6 mins | 2026-02-04 05:49:28.839Z | 203.941° SW | 2026-02-04 05:51:28.839Z | 248.917° W | 31.568° | 2026-02-04 05:55:28.839Z | 330.378° 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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