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IRIDE-MS2-HEO-02

In orbit NORAD 64569 GLPZ-0943-1414-0560-0702 ESA Italy

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IRIDE-MS2-HEO-02
Other names
HEO 02 (a.k.a Fausto)
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
581.45 km
Apogee
583.51 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6960.6 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:39 UTC
Two-line elements (TLE)
1 64569U 25135AT  26283.94189228  .00002461  00000-0  23621-3 0  9990
2 64569 97.7859 37.0791 0001484 24.5055 335.6235 14.94004776 71166
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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 08:20:48 IRIDE-MS2-HEO-2
NORAD 64569
FENGYUN 1C DEB
NORAD 35153
4.729 14.99 7.2e-08
2026-10-11 11:17:16 APRIZESAT 8
NORAD 39425
IRIDE-MS2-HEO-2
NORAD 64569
4.851 14.90 7.0e-08
2026-10-11 16:27:57 OBJECT D
NORAD 51949
IRIDE-MS2-HEO-2
NORAD 64569
4.170 14.73 1.0e-07
2026-10-12 03:02:25 IRIDE-MS2-HEO-2
NORAD 64569
FOREST-16 (SOWITASGOHT)
NORAD 68998
3.489 14.16 1.7e-07
2026-10-15 06:06:14 PERSEUS-M1
NORAD 40039
IRIDE-MS2-HEO-2
NORAD 64569
3.097 14.89 1.7e-07
2026-10-15 21:14:01 IRIDE-MS2-HEO-2
NORAD 64569
COSMOS 2251 DEB
NORAD 40799
1.962 14.55 4.8e-07
2026-10-16 14:10:59 IRIDE-MS2-HEO-2
NORAD 64569
CZ-6A DEB
NORAD 60883
2.118 15.08 3.4e-07
2026-10-16 17:23:22 IRIDE-MS2-HEO-2
NORAD 64569
LEMUR-2-CLARA
NORAD 68483
3.185 14.67 1.8e-07
2026-10-16 18:59:50 IRIDE-MS2-HEO-2
NORAD 64569
LEMUR-2-CLARA
NORAD 68483
3.377 14.67 1.6e-07
2026-10-16 19:48:04 IRIDE-MS2-HEO-2
NORAD 64569
LEMUR-2-CLARA
NORAD 68483
4.113 14.65 1.1e-07
2026-10-16 21:24:32 IRIDE-MS2-HEO-2
NORAD 64569
LEMUR-2-CLARA
NORAD 68483
1.620 14.65 6.8e-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