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ION SCV Charismatic Carlus

In orbit NORAD 64575 MJWC-6105-7146-5103-2066

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

23

Observations all time

Mission information
Spacecraft name
ION SCV Charismatic Carlus
Other names
ION SCV-018
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
2025-06-23 21:25:00
Separation time
2025-06-23 23:45:40
Last observers
Observer
Time of receipt
2025-06-25 21:22:48 UTC
2025-06-25 21:20:46 UTC
2025-06-25 18:08:46 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
572.23 km
Apogee
587.70 km
Inclination
97.8°
Period
96.3 min
Semi-major axis
6958.1 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 64575U 25135AZ  26282.76045562  .00000389  00000-0  41029-4 0  9998
2 64575 97.7888 36.8970 0011117 271.3744 88.6203 14.94813975 71048
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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
2026-10-10 23:40:22 ION SCV-018
NORAD 64575
COSMOS 886 DEB
NORAD 9819
4.202 12.69 1.5e-07
2026-10-11 03:35:55 SATELIOT_1
NORAD 60550
ION SCV-018
NORAD 64575
2.140 5.15 9.1e-07
2026-10-11 17:57:49 EZIE-C
NORAD 63249
ION SCV-018
NORAD 64575
1.890 13.89 6.2e-07
2026-10-11 22:12:59 ION SCV-018
NORAD 64575
MIMIR 1
NORAD 68490
3.567 14.71 1.4e-07
2026-10-12 05:23:59 ION SCV-018
NORAD 64575
COSMOS 2251 DEB
NORAD 34909
3.963 14.89 1.1e-07
2026-10-12 10:48:41 ION SCV-018
NORAD 64575
ET-001C
NORAD 69942
3.068 14.29 2.1e-07
2026-10-12 10:49:14 ION SCV-018
NORAD 64575
NULINK-2
NORAD 68994
3.552 14.14 1.7e-07
2026-10-12 23:55:15 ION SCV-018
NORAD 64575
IO-1
NORAD 68498
1.249 14.71 1.1e-06
2026-10-12 23:56:57 ION SCV-018
NORAD 64575
CZ-6A DEB
NORAD 60848
4.020 15.11 9.4e-08
2026-10-13 04:37:06 YAOGAN-3
NORAD 32289
ION SCV-018
NORAD 64575
3.985 10.16 2.2e-07
2026-10-13 07:00:46 ION SCV-018
NORAD 64575
CZ-6A DEB
NORAD 55196
3.013 3.73 4.7e-07
2026-10-13 16:42:26 ION SCV-018
NORAD 64575
UNKNOWN
NORAD 82494
2.369 10.70 5.9e-07
2026-10-14 00:01:02 ION SCV-018
NORAD 64575
BLACK KITE-2
NORAD 68474
2.127 14.70 3.9e-07
2026-10-14 06:26:34 ION SCV-018
NORAD 64575
TORO-3
NORAD 68481
3.223 14.70 1.7e-07
2026-10-14 09:24:05 ION SCV-018
NORAD 64575
ET-001D
NORAD 100100
4.145 14.29 1.2e-07
2026-10-14 13:26:35 ION SCV-018
NORAD 64575
PSLV DEB
NORAD 27655
1.886 13.87 6.3e-07
2026-10-14 23:51:36 ION SCV-018
NORAD 64575
GRITSS
NORAD 69931
3.651 14.29 1.5e-07
2026-10-15 00:00:13 ION SCV-018
NORAD 64575
SL-24 DEB
NORAD 33398
4.460 10.77 1.6e-07
2026-10-16 02:11:52 ION SCV-018
NORAD 64575
ELECTRON KICK STAGE R/B
NORAD 100244
2.894 8.31 4.5e-07
2026-10-16 06:27:34 ION SCV-018
NORAD 64575
DELTA 1 DEB
NORAD 7890
4.112 1.45 2.6e-07
2026-10-16 08:54:58 ION SCV-018
NORAD 64575
CZ-4B DEB
NORAD 38326
3.070 7.51 4.1e-07
2026-10-16 14:25:03 ION SCV-018
NORAD 64575
KITA-36
NORAD 69909
1.808 14.28 6.2e-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