CONNECTA IOT-13, 67400
Orbit data source: Space-Track
CONNECTA IOT-13, 67400 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 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: 9 hours ago
TLE from 9 hours ago
0 CONNECTA IOT-13
1 67400U 26004AP 26146.51508308 .00013329 00000-0 66082-3 0 9991
2 67400 97.4559 145.8352 0010520 70.4895 289.7474 15.17813825 20461Epoch: 2026-05-26T12:21Z
TLE epoch observation values (Epoch: 2026-05-26T12:21:43.178Z)
Latitude
-0.00002°
Longitude
76.31788°
Altitude
513.092 km
Speed
7.609 km/s
True Right ascension
09h 43m 20s
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
06:44:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.666 km
Perigee altitude
502.174 km
Semi-major axis
6,887.557 km
Eccentricity
0.00105
Inclination
97.4559°
RAAN
145.8352°
Arg. of periapsis
70.4895°
True anomaly
289.63389°
Mean anomaly
289.7474°
Eccentric anomaly
289.69065°
Mean motion
3.79704 °/min
Orbital period
94.81 mins
BSTAR
0.00066082
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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-13 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 23:34:41.092Z | 136.812° SSE | 2026-05-26 23:36:41.092Z | 94.464° ESE | 31.746° | 2026-05-26 23:39:41.092Z | 9.58° NNE |
| 5 mins | 2026-05-27 12:40:41.092Z | 25.408° NE | 2026-05-27 12:42:41.092Z | 115.583° SE | 42.214° | 2026-05-27 12:45:41.092Z | 182.582° 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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