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ConnectaIoT-3

In orbit NORAD 60475 BEFZ-9879-2316-3685-3950 Plan-S Türkiye

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

347

Observations all time

Mission information
Spacecraft name
ConnectaIoT-3
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
2024-08-16 18:56:00
Separation time
2024-08-16 19:56:08
Last observers
Observer
Time of receipt
2026-05-20 10:05:23 UTC
2026-05-19 19:44:42 UTC
2026-05-19 18:04:27 UTC
2026-05-19 10:26:51 UTC
2026-05-19 08:52:18 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
487.74 km
Apogee
490.86 km
Inclination
97.4°
Period
94.5 min
Semi-major axis
6867.4 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:19 UTC
Two-line elements (TLE)
1 60475U 24149H   26282.43226395  .00006997  00000-0  28759-3 0  9991
2 60475 97.3649 356.5126 0002265 194.3258 165.7916 15.24481824119204
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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 06:53:22 CONNECTA IOT-3
NORAD 60475
OBJECT M
NORAD 67259
2.633 0.06 6.4e-07
2026-10-14 08:56:07 CONNECTA IOT-3
NORAD 60475
SITRO-AIS-63
NORAD 67294
2.521 0.04 6.9e-07
2026-10-14 11:20:23 CONNECTA IOT-3
NORAD 60475
SL-24 DEB
NORAD 33318
1.691 13.33 8.7e-07
2026-10-15 05:02:37 CONNECTA IOT-3
NORAD 60475
SPHINX/FRAZIER
NORAD 63232
4.468 15.11 7.9e-08
2026-10-15 06:37:07 CONNECTA IOT-3
NORAD 60475
SPHINX/FRAZIER
NORAD 63232
3.514 15.11 1.3e-07
2026-10-15 06:58:36 CONNECTA IOT-3
NORAD 60475
YAOGAN-47
NORAD 66988
4.462 0.50 2.2e-07
2026-10-15 08:11:37 CONNECTA IOT-3
NORAD 60475
SPHINX/FRAZIER
NORAD 63232
3.774 15.11 1.1e-07
2026-10-15 12:07:52 CONNECTA IOT-3
NORAD 60475
SPHINX/FRAZIER
NORAD 63232
3.524 15.10 1.3e-07
2026-10-15 13:42:22 CONNECTA IOT-3
NORAD 60475
SPHINX/FRAZIER
NORAD 63232
1.365 15.10 8.4e-07
2026-10-15 15:16:52 CONNECTA IOT-3
NORAD 60475
SPHINX/FRAZIER
NORAD 63232
0.872 15.10 2.1e-06
2026-10-15 16:51:21 CONNECTA IOT-3
NORAD 60475
SPHINX/FRAZIER
NORAD 63232
3.017 15.10 1.7e-07
2026-10-15 21:07:54 CONNECTA IOT-3
NORAD 60475
BRO-18
NORAD 64550
4.834 5.20 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