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IRIDE FM8

In orbit NORAD 66702 VSBX-5054-1952-1903-8924

Observations 0
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Falcon 9 Block 5 | Transporter 15 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IRIDE FM8
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 15 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
496.45 km
Apogee
500.80 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6876.8 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:04 UTC
Two-line elements (TLE)
1 66702U 25276AN  26287.15655559  .00009443  00000-0  42393-3 0  9993
2 66702  97.4084 358.8013 0003165 348.0854  12.0307 15.21384282 48506
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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
2026-10-15 16:30:25 IRIDE-MS1-EAGLET 2-8
NORAD 66702 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		4.778 12.72 1.2e-07
2026-10-16 09:02:39 OBJECT B
NORAD 62726 		IRIDE-MS1-EAGLET 2-8
NORAD 66702 		3.766 0.04 3.1e-07
2026-10-16 11:24:03 OBJECT B
NORAD 62726 		IRIDE-MS1-EAGLET 2-8
NORAD 66702 		0.961 0.03 4.8e-06
2026-10-17 04:50:44 STARLINK-6065
NORAD 56812 		IRIDE-MS1-EAGLET 2-8
NORAD 66702 		3.155 13.38 7.5e-06
2026-10-17 05:38:07 STARLINK-6065
NORAD 56812 		IRIDE-MS1-EAGLET 2-8
NORAD 66702 		1.876 13.35 2.1e-05
2026-10-17 10:05:36 KOYOH
NORAD 58464 		IRIDE-MS1-EAGLET 2-8
NORAD 66702 		2.874 0.02 5.3e-07
2026-10-17 13:22:03 IRIDE-MS1-EAGLET 2-8
NORAD 66702 		COSMOS 2251 DEB
NORAD 36050 		4.895 9.99 1.4e-07
2026-10-20 07:07:29 IRIDE-MS1-EAGLET 2-8
NORAD 66702 		USA 40 R/B DEB
NORAD 23356 		1.176 14.85 1.6e-06
2026-10-20 17:49:26 YUNYAO-1 19
NORAD 58759 		IRIDE-MS1-EAGLET 2-8
NORAD 66702 		4.048 11.39 1.9e-07
2026-10-20 18:34:52 IRIDE-MS1-EAGLET 2-8
NORAD 66702 		LPNTSAT-001 (IOD-1)
NORAD 68408 		3.512 14.98 1.3e-07
2026-10-20 19:24:09 YUNYAO-1 19
NORAD 58759 		IRIDE-MS1-EAGLET 2-8
NORAD 66702 		3.286 11.42 2.9e-07
2026-10-20 23:55:54 TOMORROW-S5
NORAD 63234 		IRIDE-MS1-EAGLET 2-8
NORAD 66702 		2.110 15.10 3.5e-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