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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
564.89 km
Apogee
574.76 km
Inclination
97.5°
Period
96.1 min
Semi-major axis
6948.0 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 66682U 25276S   26284.14534740  .00001437  00000-0  12612-3 0  9990
2 66682 97.5186 350.6366 0007106 129.0279 231.1577 14.98080683 47430
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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
2026-10-11 21:21:25 ION SCV-022
NORAD 66682
STARLINK-35763
NORAD 67089
2.123 14.88 1.1e-05
2026-10-12 05:26:12 STARLINK-5642
NORAD 55430
ION SCV-022
NORAD 66682
4.541 9.44 5.2e-06
2026-10-13 22:59:26 ION SCV-022
NORAD 66682
STARLINK-35882
NORAD 67088
3.395 15.00 4.2e-06
2026-10-14 01:16:19 ION SCV-022
NORAD 66682
FENGYUN 1C DEB
NORAD 29816
1.093 15.07 1.3e-06
2026-10-14 04:49:02 ION SCV-022
NORAD 66682
CZ-4C DEB
NORAD 44616
3.980 2.36 2.8e-07
2026-10-14 18:09:14 ION SCV-022
NORAD 66682
STARLINK-36239
NORAD 67196
2.881 3.90 1.6e-05
2026-10-14 20:33:34 ION SCV-022
NORAD 66682
STARLINK-36239
NORAD 67196
4.246 3.92 7.2e-06
2026-10-15 02:59:24 ION SCV-022
NORAD 66682
STARLINK-36200
NORAD 67101
3.129 15.02 4.8e-06
2026-10-15 12:23:31 FORMOSAT 7-2
NORAD 44351
ION SCV-022
NORAD 66682
2.186 10.35 7.1e-07
2026-10-16 01:22:43 ION SCV-022
NORAD 66682
STARLINK-36236
NORAD 67078
2.403 15.05 8.1e-06
2026-10-16 09:30:46 STARLINK-5270
NORAD 55299
ION SCV-022
NORAD 66682
3.735 14.96 3.5e-06
2026-10-16 10:18:53 STARLINK-5270
NORAD 55299
ION SCV-022
NORAD 66682
1.170 14.99 3.5e-05
2026-10-16 11:33:40 ION SCV-022
NORAD 66682
CZ-6A R/B
NORAD 67434
3.562 10.07 2.7e-07
2026-10-16 20:06:08 ION SCV-022
NORAD 66682
SPOT 2
NORAD 20436
4.223 11.52 3.5e-06
2026-10-17 01:55:10 TRITON-1
NORAD 39427
ION SCV-022
NORAD 66682
4.773 14.77 7.6e-08

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