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ION SCV Passionate Paula

In orbit NORAD 64545 JLJE-0670-3801-0857-8118

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

16

Observations all time

Mission information
Spacecraft name
ION SCV Passionate Paula
Other names
ION SCV-020
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 22:23:22
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
497.22 km
Apogee
509.76 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6881.6 km
Velocity
7.6 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-07 20:46:52 UTC
Two-line elements (TLE)
1 64545U 25135T   26280.31266708  .00002140  00000-0  10315-3 0  9991
2 64545 97.4707 33.9830 0009110 116.7708 243.4460 15.19775098 71875
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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 18:57:42 ION SCV-020
NORAD 64545
FRONTIERSAT
NORAD 69015
3.270 14.30 1.9e-07
2026-10-12 23:00:58 OBJECT F
NORAD 61899
ION SCV-020
NORAD 64545
4.936 5.77 1.7e-07
2026-10-12 23:01:29 AISTECHSAT 2
NORAD 43768
ION SCV-020
NORAD 64545
4.110 8.43 2.2e-07
2026-10-13 10:59:40 ION SCV-020
NORAD 64545
IRIDE-MS1-EAGLET 2-14
NORAD 68447
2.869 14.79 2.2e-07
2026-10-13 12:34:27 ION SCV-020
NORAD 64545
IRIDE-MS1-EAGLET 2-14
NORAD 68447
4.325 14.79 9.5e-08
2026-10-13 13:23:20 SPACEMOBILE-001
NORAD 61047
ION SCV-020
NORAD 64545
4.000 10.77 2.1e-07
2026-10-13 18:02:58 LEMUR-2-ESPERANZA
NORAD 63352
ION SCV-020
NORAD 64545
2.322 14.09 4.0e-07
2026-10-14 02:00:31 ION SCV-020
NORAD 64545
DB GME UT (DB-GLOBE MISSION EARTH-UT)
NORAD 68459
4.558 14.75 8.5e-08
2026-10-14 03:35:22 ION SCV-020
NORAD 64545
DB GME UT (DB-GLOBE MISSION EARTH-UT)
NORAD 68459
4.890 14.75 7.4e-08
2026-10-14 12:54:57 ION SCV-020
NORAD 64545
RASSVET-3 9
NORAD 68368
3.350 14.69 1.6e-07
2026-10-15 01:08:16 YAOGAN-36 05B
NORAD 57454
ION SCV-020
NORAD 64545
1.524 7.99 1.7e-06
2026-10-15 02:43:09 YAOGAN-36 05B
NORAD 57454
ION SCV-020
NORAD 64545
2.921 7.98 4.5e-07
2026-10-15 05:16:12 ION SCV-020
NORAD 64545
FALCON 9 DEB
NORAD 48610
4.657 14.45 9.1e-08
2026-10-15 11:11:32 ION SCV-020
NORAD 64545
HOTSAT-2
NORAD 68465
2.841 14.75 2.2e-07
2026-10-17 08:51:47 ION SCV-020
NORAD 64545
RASSVET-3 12
NORAD 68371
2.172 14.79 3.7e-07
2026-10-17 08:53:09 OBJECT P
NORAD 61907
ION SCV-020
NORAD 64545
4.943 5.61 1.7e-07
2026-10-17 11:09:11 ION SCV-020
NORAD 64545
EYCORE-1
NORAD 69011
3.174 14.28 2.0e-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