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IRIDE-MS2-HEO-08

In orbit NORAD 64587 XQOO-5836-8962-0849-4671 ESA Italy

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IRIDE-MS2-HEO-08
Other names
HEO-08 (a.k.a Giorgiovanna Fumotto)
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 23:44:02
Satellite appearance
Operator
ESA
Data for the last 30 days
Orbital parameters of the satellite
Perigee
587.71 km
Apogee
589.72 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6966.9 km
Velocity
7.55 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:44 UTC
Two-line elements (TLE)
1 64587U 25135BM  26280.94577016  .00001258  00000-0  12960-3 0  9990
2 64587 97.7835 33.9633 0001438 57.1258 303.0099 14.92001321 70714
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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 00:23:10 IRIDE-MS2-HEO-8
NORAD 64587
CZ-2D DEB
NORAD 44612
2.292 12.46 5.3e-07
2026-10-11 04:30:26 IRIDE-MS2-HEO-8
NORAD 64587
MIMIR 1
NORAD 68490
2.829 14.68 2.2e-07
2026-10-11 06:07:02 IRIDE-MS2-HEO-8
NORAD 64587
MIMIR 1
NORAD 68490
3.727 14.68 1.3e-07
2026-10-11 06:55:21 IRIDE-MS2-HEO-8
NORAD 64587
MIMIR 1
NORAD 68490
4.598 14.65 8.4e-08
2026-10-11 09:01:42 IRIDE-MS2-HEO-8
NORAD 64587
COSMOS 2251 DEB
NORAD 47069
3.232 15.01 1.5e-07
2026-10-12 00:37:38 IRIDE-MS2-HEO-8
NORAD 64587
UNICORN-2R
NORAD 68477
1.053 14.65 1.6e-06
2026-10-12 20:40:40 O/OREOS (USA 219)
NORAD 37224
IRIDE-MS2-HEO-8
NORAD 64587
2.229 13.97 4.4e-07
2026-10-13 08:34:07 IRIDE-MS2-HEO-8
NORAD 64587
FLORBELA
NORAD 100529
3.890 14.25 1.3e-07
2026-10-13 10:10:40 IRIDE-MS2-HEO-8
NORAD 64587
FLORBELA
NORAD 100529
4.577 14.25 9.6e-08
2026-10-13 10:37:24 IRIDE-MS2-HEO-8
NORAD 64587
COSMOS 2251 DEB
NORAD 34681
1.598 3.19 1.7e-06
2026-10-14 17:20:54 IRIDE-MS2-HEO-8
NORAD 64587
SPIRONE
NORAD 66657
4.117 14.97 9.4e-08
2026-10-15 14:16:14 IRIDE-MS2-HEO-8
NORAD 64587
JACK K
NORAD 66659
3.456 14.97 1.3e-07
2026-10-16 06:21:52 IRIDE-MS2-HEO-8
NORAD 64587
COSMIC
NORAD 66658
2.962 14.97 1.8e-07
2026-10-16 23:29:17 IRIDE-MS2-HEO-8
NORAD 64587
YAM-13
NORAD 68993
4.953 14.16 8.4e-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