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ConnectaIoT-13

In orbit NORAD 67400 CACA-5365-2238-5606-7993 Plan-S Türkiye

Time in UTC

01:37

Next pass · Обозерский

—

No observations scheduled

2

Observations over 30 days

68%

Successful observations

2k

Frames, latest 2026-08-10 03:27 UTC

Mission information
Spacecraft name
ConnectaIoT-13
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-01-11 13:18:59
Separation time
2026-01-11 13:18:59
Last observers
Observer
Time of receipt
2026-08-10 03:27:53 UTC
2026-08-05 03:15:25 UTC
2026-08-04 03:31:28 UTC
2026-08-03 14:33:00 UTC
2026-06-19 14:05:11 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
501.38 km
Apogee
510.77 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6884.2 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 67400U 26004AP  26284.25933632  .00009168  00000-0  44192-3 0  9991
2 67400 97.4632 281.6824 0006770 317.7868 42.2844 15.18923939 41369
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 08:43:07 CONNECTA IOT-13
NORAD 67400
COSMO
NORAD 68460
3.518 5.23 3.4e-07
2026-10-12 13:15:42 STARLINK-1522
NORAD 46027
CONNECTA IOT-13
NORAD 67400
4.594 8.94 5.3e-06
2026-10-12 15:38:02 STARLINK-1522
NORAD 46027
CONNECTA IOT-13
NORAD 67400
2.131 9.00 2.4e-05
2026-10-13 16:18:10 TRANSPORTER-15 OBJECT CY
NORAD 66760
CONNECTA IOT-13
NORAD 67400
3.987 9.11 2.3e-07
2026-10-14 10:58:52 YAOGAN-39 01B
NORAD 57728
CONNECTA IOT-13
NORAD 67400
4.237 13.71 1.3e-07
2026-10-14 11:46:16 YAOGAN-39 01B
NORAD 57728
CONNECTA IOT-13
NORAD 67400
4.925 13.72 9.6e-08
2026-10-14 22:19:58 CONNECTA IOT-13
NORAD 67400
PSLV DEB
NORAD 27136
3.940 10.49 2.2e-07
2026-10-15 13:21:42 CONNECTA IOT-13
NORAD 67400
TRANSPORTER-18 OBJECT C
NORAD 100885
4.678 8.85 1.7e-07
2026-10-16 09:07:24 FLOCK 4H-4
NORAD 66707
CONNECTA IOT-13
NORAD 67400
4.608 9.09 1.7e-07
2026-10-17 11:51:07 CONNECTA IOT-13
NORAD 67400
COSMOS 970 DEB
NORAD 20032
2.280 6.72 7.7e-07
2026-10-17 19:55:36 HYDRA-2
NORAD 67389
CONNECTA IOT-13
NORAD 67400
1.779 0.03 1.4e-06
2026-10-17 20:42:34 HYDRA-2
NORAD 67389
CONNECTA IOT-13
NORAD 67400
4.934 0.03 1.8e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite