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ConnectaIoT-15

In orbit NORAD 67402 JWOD-9905-9321-9779-5407 Plan-S Türkiye

Time in UTC

01:59

Next pass · Обозерский

12.10 03:34

Scheduled · Сампо-400 [R1NAV]

128

Observations over 30 days

82%

Successful observations

12k

Frames, latest 2026-10-11 14:49 UTC

Mission information
Spacecraft name
ConnectaIoT-15
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
2026-10-11 14:49:14 UTC
2026-10-11 05:31:55 UTC
2026-10-11 03:57:57 UTC
2026-10-10 15:04:15 UTC
2026-10-10 13:31:38 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
505.54 km
Apogee
507.63 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6884.7 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 67402U 26004AR  26284.27430650  .00009602  00000-0  46511-3 0  9997
2 67402 97.4634 281.5246 0001474 315.8085 44.3032 15.18755421 41345
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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 10:20:51 XINGSHIDAI 20
NORAD 58918
CONNECTA IOT-15
NORAD 67402
4.650 8.14 1.8e-07
2026-10-13 15:34:08 CONNECTA IOT-15
NORAD 67402
THOR ABLESTAR DEB
NORAD 461
2.030 15.09 3.8e-07
2026-10-13 16:57:34 CONNECTA IOT-15
NORAD 67402
PIESAT-2 OBJECT D
NORAD 100752
4.542 15.04 7.7e-08
2026-10-14 17:58:45 SDGSAT 1
NORAD 49387
CONNECTA IOT-15
NORAD 67402
4.564 5.78 2.0e-07
2026-10-14 21:01:24 STARLINK-6065
NORAD 56812
CONNECTA IOT-15
NORAD 67402
3.053 14.76 5.8e-06
2026-10-15 04:14:40 MICE-1
NORAD 66684
CONNECTA IOT-15
NORAD 67402
2.677 9.12 5.1e-07
2026-10-15 15:31:16 CONNECTA IOT-15
NORAD 67402
COSMOS 2251 DEB
NORAD 36551
3.280 15.12 1.4e-07
2026-10-16 10:18:03 SJ-12
NORAD 36596
CONNECTA IOT-15
NORAD 67402
1.071 3.07 3.8e-06
2026-10-17 13:10:59 OBJECT E
NORAD 59921
CONNECTA IOT-15
NORAD 67402
3.401 2.40 3.8e-07
2026-10-17 21:53:52 CONNECTA IOT-15
NORAD 67402
OPTISAT
NORAD 68418
2.382 5.15 7.4e-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