CONNECTA IOT-16, 67390
Orbit data source: Space-Track
CONNECTA IOT-16, 67390 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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67390 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: 6 hours ago
TLE from 6 hours ago
0 CONNECTA IOT-16
1 67390U 26004AD 26146.55705517 .00002974 00000-0 15067-3 0 9995
2 67390 97.4582 145.8213 0005627 69.1169 291.0667 15.17740837 20464Epoch: 2026-05-26T13:22Z
TLE epoch observation values (Epoch: 2026-05-26T13:22:09.566Z)
Latitude
-0.00001°
Longitude
61.15266°
Altitude
514.364 km
Speed
7.607 km/s
True Right ascension
09h 43m 17s
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
04:32:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.517 km
Perigee altitude
505.765 km
Semi-major axis
6,887.778 km
Eccentricity
0.00056
Inclination
97.4582°
RAAN
145.8213°
Arg. of periapsis
69.1169°
True anomaly
291.00651°
Mean anomaly
291.0667°
Eccentric anomaly
291.03661°
Mean motion
3.79686 °/min
Orbital period
94.82 mins
BSTAR
0.00015067
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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-16 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-26 23:01:34.631Z | 98.69° ESE | 2026-05-26 23:03:34.631Z | 61.612° ENE | 15.673° | 2026-05-26 23:05:34.631Z | 28.585° NE |
| 4 mins | 2026-05-27 00:35:34.631Z | 222.91° SW | 2026-05-27 00:36:34.631Z | 248.57° W | 26.071° | 2026-05-27 00:39:34.631Z | 319.419° NNW |
| 4 mins | 2026-05-27 12:06:34.631Z | 55.222° ENE | 2026-05-27 12:08:34.631Z | 99.878° ESE | 21.784° | 2026-05-27 12:10:34.631Z | 140.783° SSE |
| 4 mins | 2026-05-27 13:40:34.631Z | 325.856° NNW | 2026-05-27 13:42:34.631Z | 283.673° WNW | 19.336° | 2026-05-27 13:44:34.631Z | 247.102° WSW |
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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