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ConnectaIoT-10

In orbit NORAD 64555 OPSM-5371-6840-8894-7677 Plan-S Türkiye

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

133

Observations all time

Mission information
Spacecraft name
ConnectaIoT-10
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 22:19:41
Last observers
Observer
Time of receipt
2026-05-20 11:20:39 UTC
2026-05-18 22:45:19 UTC
2026-05-18 11:57:09 UTC
2026-05-17 23:04:04 UTC
2026-05-17 21:29:08 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
498.29 km
Apogee
498.95 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6876.8 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:39 UTC
Two-line elements (TLE)
1 64555U 25135AD  26283.96187415  .00010974  00000-0  49210-3 0  9993
2 64555 97.4791 38.0219 0000484 117.8145 242.3140 15.21387538 72457
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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
2026-10-11 11:48:53 CONNECTA IOT-10
NORAD 64555
IRIDIUM 33 DEB
NORAD 40996
4.688 15.22 6.7e-08
2026-10-11 12:54:31 CONNECTA IOT-10
NORAD 64555
ALSAT-3B
NORAD 67646
4.396 5.29 2.2e-07
2026-10-12 22:49:46 CONNECTA IOT-10
NORAD 64555
OBJECT A
NORAD 67746
4.098 1.79 2.6e-07
2026-10-13 07:56:59 CONNECTA IOT-10
NORAD 64555
HULIANWANG JISHU SHIYAN 10A
NORAD 69320
3.972 14.78 1.1e-07
2026-10-13 20:11:17 OBJECT A
NORAD 61238
CONNECTA IOT-10
NORAD 64555
4.693 12.18 1.3e-07
2026-10-14 04:28:51 HULIANWANG JISHU SHIYAN 6C
NORAD 63430
CONNECTA IOT-10
NORAD 64555
4.651 14.77 8.3e-08
2026-10-14 05:30:19 KANOPUS-V-IK
NORAD 42825
CONNECTA IOT-10
NORAD 64555
2.495 14.52 3.1e-07
2026-10-14 10:21:44 CONNECTA IOT-10
NORAD 64555
IRIDE-MS1-EAGLET 2-1
NORAD 66695
2.543 5.40 6.4e-07
2026-10-14 11:09:05 CONNECTA IOT-10
NORAD 64555
IRIDE-MS1-EAGLET 2-1
NORAD 66695
4.633 5.41 1.9e-07
2026-10-14 19:10:33 CONNECTA IOT-10
NORAD 64555
ERMIS-1
NORAD 68468
2.893 14.80 2.1e-07
2026-10-15 10:49:42 CONNECTA IOT-10
NORAD 64555
IRIDE-MS1-EAGLET 2-3
NORAD 66697
4.323 5.42 2.2e-07
2026-10-16 02:40:12 CONNECTA IOT-10
NORAD 64555
SL-3 DEB
NORAD 25655
3.468 13.71 1.9e-07
2026-10-17 06:16:31 CONNECTA IOT-10
NORAD 64555
HAWK-13C
NORAD 67393
3.422 12.79 2.3e-07
2026-10-17 07:09:17 CONNECTA IOT-10
NORAD 64555
ERMIS-3
NORAD 68425
4.719 14.79 8.0e-08
2026-10-17 07:56:40 CONNECTA IOT-10
NORAD 64555
ERMIS-3
NORAD 68425
4.759 14.76 7.8e-08

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