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ConnectaIoT-4

In orbit NORAD 60524 QMTG-4209-6674-7825-1293 Plan-S Türkiye

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

322

Observations all time

Mission information
Spacecraft name
ConnectaIoT-4
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 19:53:45
Last observers
Observer
Time of receipt
2026-05-19 11:22:57 UTC
2026-05-18 21:06:54 UTC
2026-05-18 19:32:19 UTC
2026-05-17 09:28:32 UTC
2026-05-16 20:48:48 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
419.12 km
Apogee
425.44 km
Inclination
97.4°
Period
93.1 min
Semi-major axis
6800.4 km
Velocity
7.66 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:40 UTC
Two-line elements (TLE)
1 60524U 24149BJ  26285.22429864  .00030506  00000-0  60326-3 0  9991
2 60524 97.3736 11.3146 0004652 209.4294 150.6694 15.47053125120396
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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
2026-10-13 07:16:56 CONNECTA IOT-4
NORAD 60524
OBJECT AU
NORAD 61777
3.712 14.55 1.4e-07
2026-10-18 02:36:37 STARLINK-2421
NORAD 48098
CONNECTA IOT-4
NORAD 60524
4.844 14.80 2.3e-06
2026-10-18 11:33:05 CONNECTA IOT-4
NORAD 60524
ELEVATION-1
NORAD 62677
4.472 0.13 2.2e-07
2026-10-18 20:17:27 STARLINK-1263
NORAD 45405
CONNECTA IOT-4
NORAD 60524
3.937 14.19 4.2e-06

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