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IRIDE FM4

In orbit NORAD 66698 RITP-8166-0494-0498-1549

Satellite appearance

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IRIDE FM4
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
501.00 km
Apogee
505.74 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6881.5 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-06-24 05:59:05 UTC
Two-line elements (TLE)
1 66698U 25276AJ  26174.93537374  .00005084  00000+0  24047-3 0  9994
2 66698 97.4183 248.2865 0003443 7.6951 352.4336 15.19812614 31442
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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
2026-10-12 01:03:54 IRIDE-MS1-EAGLET 2-4
NORAD 66698
QUBE-II
NORAD 69023
4.133 15.08 9.2e-08
2026-10-12 02:38:37 IRIDE-MS1-EAGLET 2-4
NORAD 66698
QUBE-II
NORAD 69023
1.003 15.08 1.6e-06
2026-10-12 03:07:20 SHIJIAN-6 01A (SJ-6 01A)
NORAD 28413
IRIDE-MS1-EAGLET 2-4
NORAD 66698
2.068 5.66 9.7e-07
2026-10-12 04:13:20 IRIDE-MS1-EAGLET 2-4
NORAD 66698
QUBE-II
NORAD 69023
2.975 15.08 1.8e-07
2026-10-12 11:00:33 SNUSAT-2
NORAD 43782
IRIDE-MS1-EAGLET 2-4
NORAD 66698
4.068 2.61 2.6e-07
2026-10-12 14:57:44 DRUMS
NORAD 49401
IRIDE-MS1-EAGLET 2-4
NORAD 66698
1.060 4.86 3.7e-06
2026-10-12 18:56:58 IRIDE-MS1-EAGLET 2-4
NORAD 66698
COSMO
NORAD 68460
2.775 12.72 3.5e-07
2026-10-14 00:07:14 IRIDE-MS1-EAGLET 2-4
NORAD 66698
OBJECT D
NORAD 67251
1.499 0.83 2.0e-06
2026-10-14 05:41:23 IRIDE-MS1-EAGLET 2-4
NORAD 66698
DB-WALI-WMU
NORAD 68443
3.274 12.71 2.5e-07
2026-10-14 17:53:39 ETIHAD-SAT
NORAD 63226
IRIDE-MS1-EAGLET 2-4
NORAD 66698
3.905 15.10 1.0e-07
2026-10-14 19:39:36 IRIDE-MS1-EAGLET 2-4
NORAD 66698
COSMOS 2251 DEB
NORAD 35996
2.356 15.15 2.8e-07
2026-10-14 21:25:37 SHIJIAN-26 (SJ-26)
NORAD 64199
IRIDE-MS1-EAGLET 2-4
NORAD 66698
4.060 0.84 2.7e-07
2026-10-15 09:16:25 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-35
NORAD 66738
3.773 0.07 3.1e-07
2026-10-15 10:03:39 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-35
NORAD 66738
4.583 0.07 2.1e-07
2026-10-15 13:13:01 IRIDE-MS1-EAGLET 2-4
NORAD 66698
ZIYUAN 3-04 (ZY 3-04)
NORAD 67131
3.539 0.72 3.5e-07
2026-10-15 22:23:23 IRIDE-MS1-EAGLET 2-4
NORAD 66698
THORAD AGENA D DEB
NORAD 4157
1.361 15.13 8.4e-07
2026-10-15 23:30:17 IRIDE-MS1-EAGLET 2-4
NORAD 66698
IRIDIUM 33 DEB
NORAD 40996
3.397 14.52 1.7e-07
2026-10-16 16:12:11 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-18
NORAD 66721
3.905 0.01 2.9e-07
2026-10-16 16:46:44 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-18
NORAD 66721
4.176 0.01 2.9e-07
2026-10-16 17:35:36 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-18
NORAD 66721
2.062 0.00 1.3e-06
2026-10-16 18:26:52 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-18
NORAD 66721
1.816 0.01 1.3e-06

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