CONNECTA IOT-15, 67402
Orbit data source: Space-Track
CONNECTA IOT-15, 67402 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Sun, 11 Jan 2026 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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67402 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-15
1 67402U 26004AR 26263.51868534 .00005048 00000-0 24791-3 0 9993
2 67402 97.4635 261.0336 0003804 34.0900 326.0578 15.18510063 38199Epoch: 2026-09-20T12:26Z
TLE epoch observation values (Epoch: 2026-09-20T12:26:54.413Z)
Latitude
-0°
Longitude
74.89517°
Altitude
511.255 km
Speed
7.609 km/s
True Right ascension
17h 24m 08s
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
11:32:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.932 km
Perigee altitude
504.694 km
Semi-major axis
6,885.45 km
Eccentricity
0.00038
Inclination
97.4635°
RAAN
261.0336°
Arg. of periapsis
34.09°
True anomaly
326.03345°
Mean anomaly
326.0578°
Eccentric anomaly
326.04563°
Mean motion
3.79878 °/min
Orbital period
94.77 mins
BSTAR
0.00024791
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Other satellites on launch #4 in the year 2026 (2026-01-11 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-15 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 | 2026-09-21 23:22:17.337Z | 132.922° SE | 2026-09-21 23:25:17.337Z | 79.566° E | 29.301° | 2026-09-21 23:28:17.337Z | 14.463° NNE |
| 5 mins | 2026-09-22 12:28:17.337Z | 33.497° NE | 2026-09-22 12:30:17.337Z | 83.377° E | 44.391° | 2026-09-22 12:33:17.337Z | 168.255° S |
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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