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IRIDE-MS1-EAGLET 2-10

In orbit NORAD 68451 DNKT-7685-3799-3371-9241

Observations 0
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Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IRIDE-MS1-EAGLET 2-10
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 16 (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
500.66 km
Apogee
503.41 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6880.2 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68451U 26067AM  26287.11593712  .00008277  00000-0  38446-3 0  9991
2 68451  97.4660 244.1246 0001997  37.6694 322.4681 15.20256390 30004
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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 21:00:47 IRIDE-MS1-EAGLET 2-10
NORAD 68451 		CAMOES
NORAD 68507 		2.391 0.02 7.7e-07
2026-10-15 21:48:20 IRIDE-MS1-EAGLET 2-10
NORAD 68451 		CAMOES
NORAD 68507 		1.879 0.02 1.3e-06
2026-10-16 08:37:58 OBJECT C
NORAD 67748 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		4.533 15.05 7.8e-08
2026-10-16 10:12:46 OBJECT C
NORAD 67748 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		4.802 15.05 7.0e-08
2026-10-16 11:59:39 OBJECT AD
NORAD 67275 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		2.606 12.78 4.0e-07
2026-10-16 23:48:31 STARLINK-6198
NORAD 56768 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		4.700 13.32 3.4e-06
2026-10-17 00:36:09 OUT OF THE BOX (OOTB)
NORAD 68428 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		3.967 0.01 2.5e-07
2026-10-18 22:49:38 OBJECT A
NORAD 63291 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		4.716 15.09 7.1e-08
2026-10-19 10:53:11 STARLINK-5925
NORAD 55945 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		2.467 15.09 7.8e-06
2026-10-20 01:24:27 IRIDE-MS1-EAGLET 2-10
NORAD 68451 		SL-3 R/B
NORAD 12904 		3.272 7.82 9.9e-07
2026-10-20 15:15:26 STARLINK-5862
NORAD 55920 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		3.999 15.12 2.9e-06
2026-10-20 17:05:25 OBJECT AG
NORAD 67278 		IRIDE-MS1-EAGLET 2-10
NORAD 68451 		3.943 12.77 1.7e-07
2026-10-20 17:54:39 IRIDE-MS1-EAGLET 2-10
NORAD 68451 		RASSVET-3 30
NORAD 100096 		4.963 13.19 1.0e-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