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ConnectaIoT-12

In orbit NORAD 64553 XXEA-0494-6151-7239-4386 Plan-S Türkiye

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

218

Observations all time

Mission information
Spacecraft name
ConnectaIoT-12
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-06-23 21:25:00
Separation time
2025-06-23 22:20:13
Last observers
Observer
Time of receipt
2026-06-05 10:53:07 UTC
2026-05-19 22:13:03 UTC
2026-05-19 11:29:10 UTC
2026-05-18 22:34:31 UTC
2026-05-18 11:45:44 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
497.63 km
Apogee
499.65 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6876.8 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:58 UTC
Two-line elements (TLE)
1 64553U 25135AB  26283.54863553  .00008173  00000-0  36748-3 0  9999
2 64553 97.4851 38.1848 0001468 50.8310 309.3056 15.21382833 72402
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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 07:37:04 CONNECTA IOT-12
NORAD 64553
CZ-2C DEB
NORAD 37735
1.081 14.96 1.4e-06
2026-10-12 23:11:19 CONNECTA IOT-12
NORAD 64553
LEMUR-2-LAILA
NORAD 66776
4.831 5.46 1.8e-07
2026-10-13 03:55:27 CONNECTA IOT-12
NORAD 64553
PHI 1
NORAD 66775
4.451 5.48 2.1e-07
2026-10-13 05:28:48 SUPERVIEW NEO-1 04
NORAD 63126
CONNECTA IOT-12
NORAD 64553
3.096 0.36 4.6e-07
2026-10-13 07:03:30 SUPERVIEW NEO-1 04
NORAD 63126
CONNECTA IOT-12
NORAD 64553
1.890 0.36 1.2e-06
2026-10-13 07:50:51 SUPERVIEW NEO-1 04
NORAD 63126
CONNECTA IOT-12
NORAD 64553
2.096 0.36 1.0e-06
2026-10-13 08:00:11 CONNECTA IOT-12
NORAD 64553
SHARJAH-SAT-2
NORAD 68444
4.436 14.81 9.0e-08
2026-10-13 08:47:34 CONNECTA IOT-12
NORAD 64553
SHARJAH-SAT-2
NORAD 68444
4.546 14.78 8.5e-08
2026-10-13 09:25:33 SUPERVIEW NEO-1 04
NORAD 63126
CONNECTA IOT-12
NORAD 64553
2.561 0.36 6.7e-07
2026-10-13 17:18:31 CONNECTA IOT-12
NORAD 64553
CZ-6A DEB
NORAD 56246
3.601 3.26 3.3e-07
2026-10-13 22:00:19 MALLIGYONG-1
NORAD 58400
CONNECTA IOT-12
NORAD 64553
4.290 13.30 1.4e-07
2026-10-14 00:46:30 YAOGAN-39 05C
NORAD 58559
CONNECTA IOT-12
NORAD 64553
1.833 8.12 1.1e-06
2026-10-14 12:44:39 CONNECTA IOT-12
NORAD 64553
TIANYI-52
NORAD 100742
3.875 14.73 1.2e-07
2026-10-15 12:52:55 CONNECTA IOT-12
NORAD 64553
OPTISAT
NORAD 68418
4.563 14.78 8.5e-08
2026-10-16 07:02:01 CONNECTA IOT-12
NORAD 64553
MARS-1
NORAD 68830
3.190 14.81 1.7e-07
2026-10-16 08:36:45 CONNECTA IOT-12
NORAD 64553
MARS-1
NORAD 68830
4.089 14.81 1.1e-07
2026-10-16 14:00:05 SUPERVIEW NEO-3 01
NORAD 59510
CONNECTA IOT-12
NORAD 64553
2.118 4.69 9.4e-07
2026-10-16 22:01:41 CONNECTA IOT-12
NORAD 64553
AIGLONSAT-1
NORAD 68437
3.347 14.78 1.6e-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