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

IRIDE-MS1-EAGLET 2-11

In orbit NORAD 68453 EYVJ-7333-2148-1495-2696

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IRIDE-MS1-EAGLET 2-11
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
500.54 km
Apogee
504.03 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6880.4 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 68453U 26067AP  26284.95221057  .00008945  00000-0  41605-3 0  9995
2 68453 97.4696 242.0780 0002453 24.3105 335.8245 15.20185391 29670
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
2026-10-12 21:18:48 OBJECT AE
NORAD 67276
IRIDE-MS1-EAGLET 2-11
NORAD 68453
4.351 12.77 1.4e-07
2026-10-13 07:52:04 IRIDE-MS1-EAGLET 2-11
NORAD 68453
COSMOS 374 DEB
NORAD 4699
1.023 14.91 1.6e-06
2026-10-13 22:34:11 IRIDE-MS1-EAGLET 2-11
NORAD 68453
CZ-6A DEB
NORAD 54307
2.090 13.51 5.5e-07
2026-10-14 06:28:32 IRIDE-MS1-EAGLET 2-11
NORAD 68453
TABLETSAT-AURORA
NORAD 40017
2.129 13.33 5.5e-07
2026-10-14 11:36:27 OBJECT F
NORAD 63296
IRIDE-MS1-EAGLET 2-11
NORAD 68453
1.527 15.08 6.8e-07
2026-10-14 13:30:18 CONNECTA IOT-9
NORAD 64534
IRIDE-MS1-EAGLET 2-11
NORAD 68453
0.830 14.76 2.6e-06
2026-10-14 15:05:04 CONNECTA IOT-9
NORAD 64534
IRIDE-MS1-EAGLET 2-11
NORAD 68453
4.819 14.76 7.6e-08
2026-10-14 19:13:09 IRIDE-MS1-EAGLET 2-11
NORAD 68453
NOAA 16 DEB
NORAD 41267
3.460 11.30 2.6e-07
2026-10-14 23:56:40 STARLINK-4570
NORAD 53690
IRIDE-MS1-EAGLET 2-11
NORAD 68453
1.895 10.15 2.9e-05
2026-10-15 00:44:04 STARLINK-4570
NORAD 53690
IRIDE-MS1-EAGLET 2-11
NORAD 68453
3.897 10.13 6.8e-06
2026-10-15 07:07:12 IRIDE-MS1-EAGLET 2-11
NORAD 68453
COSMOS 2251 DEB
NORAD 35905
3.679 8.14 2.8e-07
2026-10-15 11:44:42 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
2.596 7.41 5.8e-07
2026-10-15 13:19:28 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
0.912 7.41 4.7e-06
2026-10-15 14:54:15 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
4.404 7.41 2.0e-07
2026-10-16 01:10:20 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
2.562 7.42 6.0e-07
2026-10-16 02:45:07 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
1.582 7.42 1.6e-06
2026-10-16 04:19:54 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
4.747 7.42 1.7e-07
2026-10-17 00:50:13 VEERY-0G
NORAD 66675
IRIDE-MS1-EAGLET 2-11
NORAD 68453
4.498 12.71 1.3e-07
2026-10-17 03:59:44 SITRO-AIS-60
NORAD 67260
IRIDE-MS1-EAGLET 2-11
NORAD 68453
3.987 12.76 1.7e-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