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: 8 hours ago
TLE from 8 hours ago
0 CONNECTA IOT-5
1 62703U 25009CY 25286.45618518 .00002068 00000-0 19980-3 0 9991
2 62703 97.7248 4.4430 0003154 136.1860 223.9611 14.93890898 40524Epoch: 2025-10-13T10:56Z
TLE epoch observation values (Epoch: 2025-10-13T10:56:54.399Z)
Latitude
0°
Longitude
177.95763°
Altitude
590.445 km
Speed
7.564 km/s
True Right ascension
00h 17m 46s
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
13:48:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.027 km
Perigee altitude
580.636 km
Semi-major axis
6,960.969 km
Eccentricity
0.00032
Inclination
97.7248°
RAAN
4.443°
Arg. of periapsis
136.186°
True anomaly
223.93602°
Mean anomaly
223.9611°
Eccentric anomaly
223.94856°
Mean motion
3.73713 °/min
Orbital period
96.33 mins
BSTAR
0.0001998
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-14 04:46:54.465Z | 124.42° SE | 2025-10-14 04:48:54.465Z | 79.288° E | 29.738° | 2025-10-14 04:51:54.465Z | 12.958° NNE |
| 7 mins | 2025-10-14 18:03:54.465Z | 18.747° NNE | 2025-10-14 18:06:54.465Z | 94.336° ESE | 43.534° | 2025-10-14 18:10:54.465Z | 186.366° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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