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: 11 hours ago
TLE from 11 hours ago
0 CONNECTA IOT-15
1 67402U 26004AR 26206.44062033 .00002846 00000-0 14366-3 0 9992
2 67402 97.4581 204.7371 0003407 165.1255 195.0079 15.17912895 29536Epoch: 2026-07-25T10:34Z
TLE epoch observation values (Epoch: 2026-07-25T10:34:29.596Z)
Latitude
-0.00009°
Longitude
102.96093°
Altitude
517.503 km
Speed
7.604 km/s
True Right ascension
13h 38m 56s
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
10:25:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.467 km
Perigee altitude
506.774 km
Semi-major axis
6,887.257 km
Eccentricity
0.00034
Inclination
97.4581°
RAAN
204.7371°
Arg. of periapsis
165.1255°
True anomaly
194.99779°
Mean anomaly
195.0079°
Eccentric anomaly
195.00285°
Mean motion
3.79729 °/min
Orbital period
94.8 mins
BSTAR
0.00014366
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-25 23:22:27.348Z | 126.55° SE | 2026-07-25 23:25:27.348Z | 57.72° ENE | 25.549° | 2026-07-25 23:27:27.348Z | 17.82° NNE |
| 5 mins | 2026-07-26 12:28:27.348Z | 38.411° NE | 2026-07-26 12:30:27.348Z | 105.559° ESE | 35.201° | 2026-07-26 12:33:27.348Z | 170.923° 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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