CONNECTA IOT-14, 67401
Orbit data source: Space-Track
CONNECTA IOT-14, 67401 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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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: 7 hours ago
TLE from 7 hours ago
0 CONNECTA IOT-14
1 67401U 26004AQ 26095.51298405 .00004277 00000-0 21300-3 0 9995
2 67401 97.4516 95.6164 0008389 226.0836 133.9707 15.18088128 12733Epoch: 2026-04-05T12:18Z
TLE epoch observation values (Epoch: 2026-04-05T12:18:41.821Z)
Latitude
0.00003°
Longitude
77.12481°
Altitude
518.722 km
Speed
7.602 km/s
True Right ascension
06h 22m 27s
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
01:31:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.367 km
Perigee altitude
502.812 km
Semi-major axis
6,886.726 km
Eccentricity
0.00084
Inclination
97.4516°
RAAN
95.6164°
Arg. of periapsis
226.0836°
True anomaly
134.03983°
Mean anomaly
133.9707°
Eccentric anomaly
134.00527°
Mean motion
3.79773 °/min
Orbital period
94.79 mins
BSTAR
0.000213
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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-14 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 23:30:56.592Z | 138.894° SSE | 2026-04-05 23:33:56.592Z | 79.186° E | 31.057° | 2026-04-05 23:36:56.592Z | 9.145° NNE |
| 6 mins | 2026-04-06 12:36:56.592Z | 24.883° NE | 2026-04-06 12:38:56.592Z | 64.902° ENE | 38.754° | 2026-04-06 12:42:56.592Z | 180.555° SSW |
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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