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ION SCV-022

In orbit NORAD 66682 MGLA-5261-8948-0167-0526

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ION SCV-022
Other names
2025-276S
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
2025-11-28 00:00:00
Separation time
2025-11-28 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
564.85 km
Apogee
574.78 km
Inclination
97.5°
Period
96.1 min
Semi-major axis
6947.9 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:04 UTC
Two-line elements (TLE)
1 66682U 25276S   26286.75029919  .00001090  00000-0  96783-4 0  9993
2 66682 97.5183 353.1458 0007149 121.6226 238.5695 14.98087304 47826
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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
2026-10-14 21:39:06 HYPSO-2
NORAD 60531
ION SCV-022
NORAD 66682
1.479 1.07 2.0e-06
2026-10-15 00:34:23 ION SCV-022
NORAD 66682
STARLINK-36239
NORAD 67196
4.703 3.95 5.9e-06
2026-10-15 03:47:25 ION SCV-022
NORAD 66682
STARLINK-36166
NORAD 67084
4.548 15.04 2.3e-06
2026-10-15 17:37:02 ION SCV-022
NORAD 66682
FENGYUN 1C DEB
NORAD 31231
3.917 13.63 1.5e-07
2026-10-16 01:22:38 ION SCV-022
NORAD 66682
STARLINK-36222
NORAD 67097
4.111 15.05 2.8e-06
2026-10-16 02:10:45 ION SCV-022
NORAD 66682
STARLINK-36222
NORAD 67097
2.090 15.05 1.1e-05
2026-10-16 11:33:40 ION SCV-022
NORAD 66682
CZ-6A R/B
NORAD 67434
2.903 10.07 4.1e-07
2026-10-16 17:46:27 ION SCV-022
NORAD 66682
FENGYUN 1C DEB
NORAD 30038
1.594 9.67 1.4e-06
2026-10-16 20:06:08 ION SCV-022
NORAD 66682
SPOT 2
NORAD 20436
3.848 11.52 4.3e-06
2026-10-17 17:31:01 STARLINK-5308
NORAD 55300
ION SCV-022
NORAD 66682
3.836 15.02 3.2e-06
2026-10-17 18:15:56 ION SCV-022
NORAD 66682
SL-16 DEB
NORAD 22816
4.593 15.08 7.3e-08
2026-10-17 18:19:08 STARLINK-5308
NORAD 55300
ION SCV-022
NORAD 66682
4.867 15.03 2.0e-06
2026-10-18 10:55:51 ION SCV-022
NORAD 66682
STARLINK-36170
NORAD 67083
4.589 15.05 2.2e-06
2026-10-18 12:31:46 ION SCV-022
NORAD 66682
STARLINK-36228
NORAD 67096
3.102 15.05 4.9e-06
2026-10-18 13:48:56 ION SCV-022
NORAD 66682
TURKSAT-3USAT
NORAD 39152
2.923 3.14 5.1e-07
2026-10-18 16:42:27 STARLINK-5318
NORAD 55304
ION SCV-022
NORAD 66682
4.433 15.05 2.4e-06
2026-10-18 17:40:04 SSTL S1-4
NORAD 43618
ION SCV-022
NORAD 66682
4.187 14.77 9.8e-08
2026-10-19 09:06:12 SHIJIAN-6 05A (SJ-6 05A)
NORAD 49961
ION SCV-022
NORAD 66682
1.553 11.80 1.2e-06
2026-10-19 11:19:44 LATINSAT A
NORAD 27612
ION SCV-022
NORAD 66682
4.905 8.63 1.5e-07
2026-10-19 20:02:16 STARLINK-5502
NORAD 55644
ION SCV-022
NORAD 66682
4.382 4.38 6.7e-06
2026-10-19 21:52:10 ICEYE-X53
NORAD 64584
ION SCV-022
NORAD 66682
4.861 6.35 1.7e-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