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 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, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CONNECTA IOT-13
1 67400U 26004AP 26093.56098912 .00005087 00000-0 25963-3 0 9997
2 67400 97.4572 93.6971 0007414 241.4971 118.5517 15.17140861 12434Epoch: 2026-04-03T13:27Z
TLE epoch observation values (Epoch: 2026-04-03T13:27:49.459Z)
Latitude
0.00002°
Longitude
59.84766°
Altitude
520.018 km
Speed
7.602 km/s
True Right ascension
06h 14m 47s
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
03:52:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.567 km
Perigee altitude
506.351 km
Semi-major axis
6,889.596 km
Eccentricity
0.00074
Inclination
97.4572°
RAAN
93.6971°
Arg. of periapsis
241.4971°
True anomaly
118.62629°
Mean anomaly
118.5517°
Eccentric anomaly
118.589°
Mean motion
3.79536 °/min
Orbital period
94.85 mins
BSTAR
0.00025963
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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 | 2026-04-03 23:06:46.233Z | 110.546° ESE | 2026-04-03 23:08:46.233Z | 75.629° E | 18.089° | 2026-04-03 23:11:46.233Z | 22.621° NE |
| 5 mins | 2026-04-04 00:40:46.233Z | 216.187° SW | 2026-04-04 00:42:46.233Z | 259.024° W | 23.895° | 2026-04-04 00:45:46.233Z | 319.113° NNW |
| 5 mins | 2026-04-04 12:12:46.233Z | 51.286° ENE | 2026-04-04 12:14:46.233Z | 99.855° ESE | 25.015° | 2026-04-04 12:17:46.233Z | 155.944° SSE |
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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