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 26170.69457932 .00001074 00000-0 10559-3 0 9990
2 62703 97.7027 249.2446 0003670 70.8108 289.3510 14.94164291 77747Epoch: 2026-06-19T16:40Z
TLE epoch observation values (Epoch: 2026-06-19T16:40:11.653Z)
Latitude
0.00007°
Longitude
91.27616°
Altitude
587.168 km
Speed
7.567 km/s
True Right ascension
16h 36m 58s
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
07:22:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.535 km
Perigee altitude
579.427 km
Semi-major axis
6,960.118 km
Eccentricity
0.00037
Inclination
97.7027°
RAAN
249.2446°
Arg. of periapsis
70.8108°
True anomaly
289.31131°
Mean anomaly
289.351°
Eccentric anomaly
289.33116°
Mean motion
3.73782 °/min
Orbital period
96.31 mins
BSTAR
0.00010559
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 04:12:00.020Z | 92.599° ESE | 2026-06-21 04:14:00.020Z | 59.018° ENE | 15.316° | 2026-06-21 04:16:00.020Z | 29.325° NE |
| 6 mins | 2026-06-21 05:46:00.020Z | 199.463° SSW | 2026-06-21 05:49:00.020Z | 273.819° WNW | 32.14° | 2026-06-21 05:52:00.020Z | 328.755° NNW |
| 5 mins | 2026-06-21 17:29:00.020Z | 52.814° ENE | 2026-06-21 17:31:00.020Z | 98.215° ESE | 25.871° | 2026-06-21 17:34:00.020Z | 153.379° SSE |
| 4 mins | 2026-06-21 19:05:00.020Z | 315.752° NNW | 2026-06-21 19:06:00.020Z | 295.768° NW | 19.897° | 2026-06-21 19:09:00.020Z | 245.204° 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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