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ION SCV-002

In orbit NORAD 47504 OEYR-7835-4087-4694-0992 Italy

Observations 0
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2021

Falcon 9 Block 5 | Transporter 1 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 40

Spaceport

0

Observations all time

Mission information
Spacecraft name
ION SCV-002
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 1 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 40
Launch time
2021-01-24 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
415.52 km
Apogee
432.30 km
Inclination
97.1°
Period
93.1 min
Semi-major axis
6802.0 km
Velocity
7.66 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:18 UTC
Two-line elements (TLE)
1 47504U 21006CV  26282.91586816  .00013092  00000-0  26480-3 0  9991
2 47504  97.1177 282.5849 0012337  63.7643 296.4873 15.46493131317745
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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 23:30:37 ION SCV-002
NORAD 47504 		STARLINK-2015
NORAD 47638 		1.789 12.37 2.7e-05
2026-10-13 16:43:11 ION SCV-002
NORAD 47504 		PEGASUS DEB
NORAD 39306 		4.507 15.34 7.2e-08
2026-10-14 05:54:28 STARLINK-1133
NORAD 45064 		ION SCV-002
NORAD 47504 		2.538 6.47 1.9e-05
2026-10-14 09:47:29 STARLINK-1133
NORAD 45064 		ION SCV-002
NORAD 47504 		0.955 6.42 1.3e-04
2026-10-15 06:12:10 ION SCV-002
NORAD 47504 		CZ-6A DEB
NORAD 58433 		4.774 15.11 7.0e-08
2026-10-15 16:59:05 ION SCV-002
NORAD 47504 		STARLINK-30861
NORAD 58230 		2.477 14.37 1.0e-05

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