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ION SCV-012

In orbit NORAD 60573 LWDE-7403-4643-6587-2546

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

3

Observations all time

Mission information
Spacecraft name
ION SCV-012
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
2024-08-16 18:56:00
Separation time
2024-08-16 21:30:50
Last observers
Observer
Time of receipt
2024-09-28 21:25:36 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
575.74 km
Apogee
582.25 km
Inclination
97.7°
Period
96.3 min
Semi-major axis
6957.1 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:19 UTC
Two-line elements (TLE)
1 60573U 24149DK  26282.48478977  .00001106  00000-0  10597-3 0  9998
2 60573 97.6678 354.0468 0004677 71.4952 288.6776 14.95124048116996
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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 01:03:48 STARLINK-3109
NORAD 49143
ION SCV-012
NORAD 60573
4.300 11.56 5.0e-06
2026-10-11 03:57:54 GRUS-1B
NORAD 47934
ION SCV-012
NORAD 60573
4.700 14.92 7.4e-08
2026-10-11 15:23:51 AEROCUBE 6B
NORAD 40046
ION SCV-012
NORAD 60573
3.383 11.00 2.8e-07
2026-10-11 23:19:28 NOVASAR 1
NORAD 43619
ION SCV-012
NORAD 60573
3.790 14.68 1.2e-07
2026-10-11 23:44:46 ION SCV-012
NORAD 60573
DMSP 5D-2 F11 DEB
NORAD 28325
4.172 14.95 9.3e-08
2026-10-13 05:07:02 ION SCV-012
NORAD 60573
COSMOS 2251 DEB
NORAD 34420
4.909 13.35 1.0e-07
2026-10-13 07:40:41 STARLINK-3055
NORAD 49137
ION SCV-012
NORAD 60573
4.743 10.90 4.4e-06
2026-10-13 15:07:32 ION SCV-012
NORAD 60573
TIROS 6
NORAD 397
3.748 14.74 1.0e-07
2026-10-14 19:49:47 ION SCV-012
NORAD 60573
OBJECT B
NORAD 66651
0.761 14.24 3.5e-06
2026-10-14 23:43:03 ION SCV-012
NORAD 60573
FENGYUN 1C DEB
NORAD 29832
3.586 7.92 3.0e-07
2026-10-15 11:43:39 ION SCV-012
NORAD 60573
COSMOS 2251 DEB
NORAD 36557
3.041 13.39 2.6e-07
2026-10-16 09:06:23 ION SCV-012
NORAD 60573
COSMOS 2251 DEB
NORAD 38208
3.699 15.11 1.1e-07
2026-10-16 09:28:38 ION SCV-012
NORAD 60573
SKYKRAFT-4D
NORAD 64898
3.591 1.27 3.4e-07
2026-10-16 13:28:36 ION SCV-012
NORAD 60573
GRUS-3ALPHA
NORAD 64579
2.382 5.31 7.3e-07
2026-10-16 13:47:52 ION SCV-012
NORAD 60573
TORGA
NORAD 100802
2.998 14.98 1.8e-07
2026-10-16 22:28:31 ION SCV-012
NORAD 60573
FENGYUN 1C DEB
NORAD 37925
3.596 14.65 1.4e-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