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IRIDE-MS2-HEO-09

In orbit NORAD 64585 HBZN-9787-4481-5510-8890 ESA Italy

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IRIDE-MS2-HEO-09
Other names
HEO-09 (a.k.a Ornella Vanono)
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 23:44:12
Satellite appearance
Operator
ESA
Data for the last 30 days
Orbital parameters of the satellite
Perigee
587.75 km
Apogee
589.65 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6966.8 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:58 UTC
Two-line elements (TLE)
1 64585U 25135BK  26283.58352346  .00001563  00000-0  15971-3 0  9992
2 64585 97.7864 36.6418 0001348 57.2866 302.8483 14.92006882 71106
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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 09:03:08 IRIDE-MS2-HEO-9
NORAD 64585
COSMOS 2251 DEB
NORAD 38212
2.530 14.96 2.5e-07
2026-10-12 00:54:53 IRIDE-MS2-HEO-9
NORAD 64585
YAM-12
NORAD 69003
4.772 14.16 9.1e-08
2026-10-12 07:25:37 IRIDE-MS2-HEO-9
NORAD 64585
CZ-2D DEB
NORAD 43490
1.596 7.63 1.5e-06
2026-10-12 12:18:06 IRIDE-MS2-HEO-9
NORAD 64585
FENGYUN 1C DEB
NORAD 30971
1.398 3.17 2.2e-06
2026-10-12 17:35:58 IRIDE-MS2-HEO-9
NORAD 64585
OBJECT B
NORAD 66651
3.442 14.97 1.3e-07
2026-10-12 18:36:39 IRIDE-MS2-HEO-9
NORAD 64585
IPOS-TDSM
NORAD 69913
3.346 14.29 1.8e-07
2026-10-12 19:24:58 IRIDE-MS2-HEO-9
NORAD 64585
IPOS-TDSM
NORAD 69913
3.235 14.32 1.9e-07
2026-10-12 19:29:36 IRIDE-MS2-HEO-9
NORAD 64585
IRIDIUM 33 DEB
NORAD 35797
3.251 14.63 1.7e-07
2026-10-13 13:07:19 IRIDE-MS2-HEO-9
NORAD 64585
TOM-3
NORAD 69906
3.399 14.32 1.7e-07
2026-10-13 22:13:08 IRIDE-MS2-HEO-9
NORAD 64585
FENGYUN 1C DEB
NORAD 31296
3.931 14.51 1.2e-07
2026-10-14 05:12:24 IRIDE-MS2-HEO-9
NORAD 64585
COSMOS 886 DEB
NORAD 9653
1.119 14.10 1.8e-06
2026-10-14 07:37:53 IRIDE-MS2-HEO-9
NORAD 64585
CUBY-5
NORAD 69907
4.934 14.29 8.2e-08
2026-10-14 08:26:11 IRIDE-MS2-HEO-9
NORAD 64585
CUBY-5
NORAD 69907
1.602 14.32 7.8e-07
2026-10-14 10:15:59 UOSAT 2 (UO-11)
NORAD 14781
IRIDE-MS2-HEO-9
NORAD 64585
1.886 14.43 5.6e-07
2026-10-14 22:26:38 IRIDE-MS2-HEO-9
NORAD 64585
KUIPER-00517
NORAD 69600
4.776 14.03 9.4e-08
2026-10-15 09:23:03 IRIDE-MS2-HEO-9
NORAD 64585
CUBY-3
NORAD 69875
4.952 14.29 8.1e-08
2026-10-15 09:53:38 IRIDE-MS2-HEO-9
NORAD 64585
COSMOS 2251 DEB
NORAD 47069
4.498 15.09 7.4e-08
2026-10-15 10:11:21 IRIDE-MS2-HEO-9
NORAD 64585
CUBY-3
NORAD 69875
1.275 14.32 1.2e-06
2026-10-15 22:11:59 IRIDE-MS2-HEO-9
NORAD 64585
ESSAIM-2
NORAD 28495
3.226 14.71 1.7e-07
2026-10-15 23:48:35 IRIDE-MS2-HEO-9
NORAD 64585
ESSAIM-2
NORAD 28495
3.275 14.71 1.6e-07
2026-10-16 00:36:52 IRIDE-MS2-HEO-9
NORAD 64585
ESSAIM-2
NORAD 28495
4.981 14.73 7.1e-08
2026-10-16 02:13:28 IRIDE-MS2-HEO-9
NORAD 64585
ESSAIM-2
NORAD 28495
2.057 14.73 4.1e-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