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ConnectaIoT-14

In orbit NORAD 67401 PMIG-0045-7037-4888-4255 Plan-S Türkiye

Time in UTC

02:09

Next pass · Обозерский

—

No observations scheduled

1

Observations over 30 days

94%

Successful observations

2k

Frames, latest 2026-10-02 15:57 UTC

Mission information
Spacecraft name
ConnectaIoT-14
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
2026-10-02 15:57:47 UTC
2026-08-16 13:39:14 UTC
2026-07-19 13:43:52 UTC
2026-07-11 03:33:29 UTC
2026-07-01 03:13:35 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
498.90 km
Apogee
509.43 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6882.3 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 67401U 26004AQ  26284.21627829  .00010385  00000-0  49096-3 0  9997
2 67401 97.4575 281.6926 0007615 303.3944 56.6562 15.19553916 41376
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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 05:15:58 ZIYUAN 3-02 (ZY 3-02)
NORAD 41556
CONNECTA IOT-14
NORAD 67401
4.887 9.29 1.5e-07
2026-10-12 08:26:22 CONNECTA IOT-14
NORAD 67401
RASSVET-3 27
NORAD 100093
3.109 14.48 2.0e-07
2026-10-12 12:23:27 CONNECTA IOT-14
NORAD 67401
RASSVET-3 25
NORAD 100091
4.113 14.47 1.1e-07
2026-10-14 00:45:50 CONNECTA IOT-14
NORAD 67401
TRANSPORTER-16 OBJECT L
NORAD 68426
4.123 5.16 2.5e-07
2026-10-14 11:00:45 CONNECTA IOT-14
NORAD 67401
RASSVET-3 25
NORAD 100091
3.537 14.64 1.5e-07
2026-10-14 11:47:23 TRANSPORTER-15 OBJECT CX
NORAD 66759
CONNECTA IOT-14
NORAD 67401
2.631 9.12 5.3e-07
2026-10-15 03:49:49 CONNECTA IOT-14
NORAD 67401
CZ-4C DEB
NORAD 43266
1.961 14.97 4.3e-07
2026-10-15 10:43:04 CONNECTA IOT-14
NORAD 67401
RASSVET-3 19
NORAD 100085
2.951 14.71 2.1e-07
2026-10-15 10:45:49 S-NET D
NORAD 43186
CONNECTA IOT-14
NORAD 67401
3.694 10.97 2.4e-07
2026-10-16 01:47:07 SPACEEYE-T1
NORAD 63229
CONNECTA IOT-14
NORAD 67401
4.109 12.10 1.7e-07
2026-10-16 16:54:17 CONNECTA IOT-14
NORAD 67401
COSMOS 2251 DEB
NORAD 36551
4.964 15.07 6.4e-08
2026-10-16 19:06:03 LEO EXPRESS 2
NORAD 62673
CONNECTA IOT-14
NORAD 67401
0.795 9.14 5.8e-06
2026-10-17 10:56:25 CONNECTA IOT-14
NORAD 67401
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.302 5.21 2.3e-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