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
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 CONNECTA IOT-15
1 67402U 26004AR 26146.24796207 .00002955 00000-0 15050-3 0 9992
2 67402 97.4563 145.4348 0004988 61.8938 298.2799 15.17561744 20401Epoch: 2026-05-26T05:57Z
TLE epoch observation values (Epoch: 2026-05-26T05:57:03.922Z)
Latitude
-0.00008°
Longitude
172.34434°
Altitude
514.67 km
Speed
7.607 km/s
True Right ascension
09h 41m 44s
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
03:34:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.619 km
Perigee altitude
506.748 km
Semi-major axis
6,888.321 km
Eccentricity
0.0005
Inclination
97.4563°
RAAN
145.4348°
Arg. of periapsis
61.8938°
True anomaly
298.22955°
Mean anomaly
298.2799°
Eccentric anomaly
298.25473°
Mean motion
3.79641 °/min
Orbital period
94.83 mins
BSTAR
0.0001505
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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 | 2026-05-26 23:30:02.923Z | 132.176° SE | 2026-05-26 23:32:02.923Z | 89.633° E | 29.577° | 2026-05-26 23:35:02.923Z | 12.054° NNE |
| 5 mins | 2026-05-27 12:36:02.923Z | 29.308° NE | 2026-05-27 12:38:02.923Z | 102.7° ESE | 40.231° | 2026-05-27 12:41:02.923Z | 178.072° S |
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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