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 spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 2.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CONNECTA IOT-15
1 67402U 26004AR 26095.46682953 .00004624 00000-0 23863-3 0 9997
2 67402 97.4579 95.4418 0002523 179.0314 181.0925 15.16814183 12704Epoch: 2026-04-05T11:12Z
TLE epoch observation values (Epoch: 2026-04-05T11:12:14.071Z)
Latitude
0.00002°
Longitude
93.61133°
Altitude
520.3 km
Speed
7.602 km/s
True Right ascension
06h 21m 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
23:09:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.187 km
Perigee altitude
510.71 km
Semi-major axis
6,890.586 km
Eccentricity
0.00025
Inclination
97.4579°
RAAN
95.4418°
Arg. of periapsis
179.0314°
True anomaly
181.09195°
Mean anomaly
181.0925°
Eccentric anomaly
181.09222°
Mean motion
3.79454 °/min
Orbital period
94.87 mins
BSTAR
0.00023863
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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 | 2026-04-05 23:59:39.302Z | 167.751° S | 2026-04-06 00:02:39.302Z | 181.086° SSW | 44.719° | 2026-04-06 00:05:39.302Z | 347.302° N |
| 5 mins | 2026-04-06 13:06:39.302Z | 354.199° N | 2026-04-06 13:08:39.302Z | 295.119° NW | 38.593° | 2026-04-06 13:11:39.302Z | 211.334° SW |
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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