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IRIDE FM2

In orbit NORAD 66696 ZKZI-1167-5962-7372-0223

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 FM2
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
495.78 km
Apogee
500.07 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6876.1 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 66696U 25276AG  26282.43580896  .00004021  00000-0  18118-3 0  9997
2 66696  97.4091 354.2356 0003116 352.0245   8.0941 15.21617941 47791
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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 12:06:33 IRIDE-MS1-EAGLET 2-2
NORAD 66696 		GEN1A-2
NORAD 69005 		3.899 15.09 1.0e-07
2026-10-11 13:41:16 IRIDE-MS1-EAGLET 2-2
NORAD 66696 		GEN1A-2
NORAD 69005 		3.177 15.09 1.6e-07
2026-10-11 15:15:59 IRIDE-MS1-EAGLET 2-2
NORAD 66696 		GEN1A-2
NORAD 69005 		4.367 15.09 8.2e-08
2026-10-12 19:08:15 HXMT (HUIYAN)
NORAD 42758 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		3.601 12.40 2.2e-07
2026-10-13 10:51:41 TOMORROW-S9
NORAD 66309 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		1.434 14.08 1.1e-06
2026-10-13 23:23:37 LIZZIESAT-3 (LS-3)
NORAD 63233 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		2.722 15.10 2.1e-07
2026-10-14 00:58:17 LIZZIESAT-3 (LS-3)
NORAD 63233 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		3.693 15.10 1.1e-07
2026-10-14 03:20:18 LIZZIESAT-3 (LS-3)
NORAD 63233 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		3.881 15.09 1.0e-07
2026-10-14 04:54:58 LIZZIESAT-3 (LS-3)
NORAD 63233 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		4.488 15.09 7.8e-08
2026-10-15 13:50:44 STARLINK-6085
NORAD 57115 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		4.279 12.88 4.4e-06
2026-10-15 20:47:48 HORUS 1
NORAD 55690 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		3.294 0.04 4.1e-07
2026-10-16 00:39:38 IRIDE-MS1-EAGLET 2-2
NORAD 66696 		OBJECT B
NORAD 67747 		1.446 7.08 1.9e-06
2026-10-16 12:17:58 IRIDE-MS1-EAGLET 2-2
NORAD 66696 		HULIANWANG JISHU SHIYAN 9C
NORAD 68833 		3.318 14.33 1.8e-07
2026-10-16 20:12:15 HULIANWANG JISHU SHIYAN 6D
NORAD 63431 		IRIDE-MS1-EAGLET 2-2
NORAD 66696 		4.162 14.20 1.2e-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