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ConnectaIoT-16

In orbit NORAD 67390 XRIE-0236-5996-7855-8536 Plan-S Türkiye

Time in UTC

01:14

Next pass · Обозерский

—

No observations scheduled

4

Observations over 30 days

82%

Successful observations

2k

Frames, latest 2026-10-02 14:56 UTC

Mission information
Spacecraft name
ConnectaIoT-16
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 14:56:10 UTC
2026-08-15 13:59:02 UTC
2026-08-14 03:29:11 UTC
2026-08-05 13:32:50 UTC
2026-06-30 13:45:52 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
504.83 km
Apogee
507.86 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6884.5 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 67390U 26004AD  26283.97918799  .00009816  00000-0  47433-3 0  9995
2 67390 97.4654 281.3761 0002197 331.8631 28.2484 15.18832083 41310
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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 18:33:45 CONNECTA IOT-16
NORAD 67390
TRANSPORTER-18 OBJECT BR
NORAD 100946
4.459 8.87 1.9e-07
2026-10-12 19:21:17 OBJECT L
NORAD 61904
CONNECTA IOT-16
NORAD 67390
3.998 8.54 2.3e-07
2026-10-13 01:06:26 LEGION 5
NORAD 62900
CONNECTA IOT-16
NORAD 67390
4.830 12.21 1.2e-07
2026-10-13 02:28:06 CONNECTA IOT-16
NORAD 67390
TRANSPORTER-18 OBJECT BU
NORAD 100949
3.020 8.87 4.0e-07
2026-10-14 12:55:03 CONNECTA IOT-16
NORAD 67390
CHUBUSAT-3
NORAD 41339
1.392 8.45 1.9e-06
2026-10-15 05:03:49 CONNECTA IOT-16
NORAD 67390
SPRITE
NORAD 100954
4.442 8.87 1.9e-07
2026-10-16 04:00:07 CONNECTA IOT-16
NORAD 67390
OBJECT K
NORAD 49404
3.908 5.25 2.7e-07
2026-10-17 14:46:20 LILIUM-2
NORAD 66679
CONNECTA IOT-16
NORAD 67390
4.731 8.98 1.6e-07
2026-10-17 15:33:45 LILIUM-2
NORAD 66679
CONNECTA IOT-16
NORAD 67390
3.552 9.00 2.9e-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