RU | EN | ZH --:-- UTC Sign in
Back

IRIDE FM7

In orbit NORAD 66701 VJHD-8418-0458-7813-7824

Observations 0
Go to map
Back

—

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 FM7
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
496.25 km
Apogee
500.96 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6876.7 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:04 UTC
Two-line elements (TLE)
1 66701U 25276AM  26286.75203826  .00010874  00000-0  48740-3 0  9995
2 66701  97.4111 358.5274 0003396 320.7242  39.3747 15.21399177 48448
Copy content
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
2026-10-14 12:23:28 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		LPNTSAT-001 (IOD-1)
NORAD 68408 		3.897 14.98 1.1e-07
2026-10-15 03:38:31 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		IRIDE-MS1-EAGLET 2-12
NORAD 68461 		1.965 12.72 7.0e-07
2026-10-15 11:32:03 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		DISCO-2
NORAD 68431 		4.315 12.69 1.5e-07
2026-10-16 09:37:58 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		ION SCV-019 (ASTOUNDING ALEXANDRA)
NORAD 68435 		2.679 12.70 3.8e-07
2026-10-16 15:54:00 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		TRANSPORTER-18 OBJECT BP
NORAD 100944 		4.512 0.33 2.2e-07
2026-10-17 02:56:39 TECMS
NORAD 53346 		IRIDE-MS1-EAGLET 2-7
NORAD 66701 		3.894 0.95 2.9e-07
2026-10-17 09:15:51 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		GYEONGGISAT-2A
NORAD 100950 		4.690 0.32 2.0e-07
2026-10-18 11:19:44 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		TOMORROW-S10
NORAD 67398 		3.913 9.05 2.4e-07
2026-10-18 16:23:53 BANDWAGON-4 OBJECT D
NORAD 66296 		IRIDE-MS1-EAGLET 2-7
NORAD 66701 		3.933 14.41 1.3e-07
2026-10-19 05:04:57 SPACEEYE-T1
NORAD 63229 		IRIDE-MS1-EAGLET 2-7
NORAD 66701 		4.151 15.10 9.1e-08
2026-10-19 06:35:47 TOMORROW-S8
NORAD 66308 		IRIDE-MS1-EAGLET 2-7
NORAD 66701 		1.682 14.40 7.1e-07
2026-10-19 16:10:25 IRIDE-MS1-EAGLET 2-7
NORAD 66701 		DIADEME 1
NORAD 2674 		2.634 7.65 5.6e-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