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IRIDE-MS1-EAGLET 2-10

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

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
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
500.62 km
Apogee
503.73 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6880.3 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:37 UTC
Two-line elements (TLE)
1 68451U 26067AM  26284.68055377  .00011144  00000-0  51685-3 0  9997
2 68451 97.4651 241.7140 0002253 42.1275 318.0133 15.20220977 29634
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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 17:57:09 KOWSAR 1.5
NORAD 67264
IRIDE-MS1-EAGLET 2-10
NORAD 68451
2.450 12.80 4.5e-07
2026-10-13 08:10:14 FLOCK 4H-33
NORAD 66736
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.915 12.75 1.1e-07
2026-10-13 16:54:14 JACK-002
NORAD 68417
IRIDE-MS1-EAGLET 2-10
NORAD 68451
1.740 0.04 1.5e-06
2026-10-13 17:41:35 JACK-002
NORAD 68417
IRIDE-MS1-EAGLET 2-10
NORAD 68451
2.633 0.04 6.4e-07
2026-10-14 01:32:52 FLOCK 4H-3
NORAD 66706
IRIDE-MS1-EAGLET 2-10
NORAD 68451
1.634 12.72 1.0e-06
2026-10-14 03:55:39 ZORKIY-2M 1
NORAD 57177
IRIDE-MS1-EAGLET 2-10
NORAD 68451
2.797 11.67 3.9e-07
2026-10-14 13:24:21 IRIDE-MS1-EAGLET 2-10
NORAD 68451
OBJECT J
NORAD 51832
0.949 11.76 3.4e-06
2026-10-14 20:31:53 QB50P1
NORAD 40025
IRIDE-MS1-EAGLET 2-10
NORAD 68451
0.684 7.85 8.3e-06
2026-10-14 22:54:04 QB50P1
NORAD 40025
IRIDE-MS1-EAGLET 2-10
NORAD 68451
3.282 7.83 3.6e-07
2026-10-15 00:07:21 BLACKJACK ACES-1
NORAD 56956
IRIDE-MS1-EAGLET 2-10
NORAD 68451
2.845 15.08 1.9e-07
2026-10-15 01:42:10 BLACKJACK ACES-1
NORAD 56956
IRIDE-MS1-EAGLET 2-10
NORAD 68451
3.340 15.08 1.4e-07
2026-10-15 04:04:24 BLACKJACK ACES-1
NORAD 56956
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.566 15.09 7.5e-08
2026-10-15 23:21:18 BUZZER-1
NORAD 62609
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.426 13.02 1.3e-07
2026-10-16 01:45:30 IRIDE-MS1-EAGLET 2-10
NORAD 68451
CAMOES
NORAD 68507
2.456 0.02 7.3e-07
2026-10-16 02:32:38 IRIDE-MS1-EAGLET 2-10
NORAD 68451
CAMOES
NORAD 68507
0.442 0.02 2.3e-05
2026-10-16 14:57:12 OBJECT C
NORAD 67748
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.409 15.05 8.3e-08
2026-10-16 16:31:59 OBJECT C
NORAD 67748
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.362 15.05 8.4e-08
2026-10-17 03:01:52 IRIDE-MS1-EAGLET 2-10
NORAD 68451
RASSVET-3 19
NORAD 100085
4.557 12.71 1.3e-07
2026-10-17 03:02:13 OUT OF THE BOX (OOTB)
NORAD 68428
IRIDE-MS1-EAGLET 2-10
NORAD 68451
3.240 0.01 4.0e-07
2026-10-17 10:56:25 CONNECTA IOT-14
NORAD 67401
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.302 5.21 2.3e-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