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IRIDE-MS1-EAGLET 2-13

In orbit NORAD 68450 OUEP-4362-3382-8192-0051

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IRIDE-MS1-EAGLET 2-13
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
500.59 km
Apogee
504.31 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6880.5 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:37 UTC
Two-line elements (TLE)
1 68450U 26067AL  26284.95346464  .00009036  00000-0  42090-3 0  9993
2 68450 97.4694 242.0700 0002585 25.2450 334.8911 15.20132227 29675
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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 15:53:32 LPNTSAT-001 (IOD-1)
NORAD 68408
IRIDE-MS1-EAGLET 2-13
NORAD 68450
4.941 9.60 1.5e-07
2026-10-12 16:41:53 IRIDE-MS1-EAGLET 2-13
NORAD 68450
NOAA 16 DEB
NORAD 41267
4.990 11.33 1.3e-07
2026-10-13 09:48:43 IRIDE-MS1-EAGLET 2-13
NORAD 68450
CZ-6A DEB
NORAD 54523
3.493 14.99 1.4e-07
2026-10-13 21:29:55 BLACKJACK ACES-2
NORAD 56955
IRIDE-MS1-EAGLET 2-13
NORAD 68450
1.916 15.08 4.3e-07
2026-10-13 23:04:44 BLACKJACK ACES-2
NORAD 56955
IRIDE-MS1-EAGLET 2-13
NORAD 68450
2.905 15.08 1.9e-07
2026-10-14 15:50:00 FEMTO-1
NORAD 68419
IRIDE-MS1-EAGLET 2-13
NORAD 68450
4.164 0.00 1.3e-07
2026-10-14 16:40:17 FEMTO-1
NORAD 68419
IRIDE-MS1-EAGLET 2-13
NORAD 68450
3.294 0.01 4.1e-07
2026-10-14 20:44:16 ZORKY-2M 7
NORAD 67268
IRIDE-MS1-EAGLET 2-13
NORAD 68450
2.434 12.78 4.6e-07
2026-10-14 23:06:48 OBJECT D
NORAD 66056
IRIDE-MS1-EAGLET 2-13
NORAD 68450
4.623 12.26 1.3e-07
2026-10-14 23:54:11 OBJECT D
NORAD 66056
IRIDE-MS1-EAGLET 2-13
NORAD 68450
2.527 12.28 4.5e-07
2026-10-15 00:41:36 OBJECT D
NORAD 66056
IRIDE-MS1-EAGLET 2-13
NORAD 68450
1.947 12.26 7.6e-07
2026-10-15 01:28:59 OBJECT D
NORAD 66056
IRIDE-MS1-EAGLET 2-13
NORAD 68450
4.034 12.28 1.8e-07
2026-10-15 11:20:06 OBJECT F
NORAD 63296
IRIDE-MS1-EAGLET 2-13
NORAD 68450
4.870 15.08 6.7e-08
2026-10-15 12:54:56 OBJECT F
NORAD 63296
IRIDE-MS1-EAGLET 2-13
NORAD 68450
2.790 15.08 2.0e-07
2026-10-15 22:00:06 IRIDE-MS1-EAGLET 2-13
NORAD 68450
TABLETSAT-AURORA
NORAD 40017
0.491 13.34 1.0e-05
2026-10-16 07:52:14 YAOGAN-36 05C
NORAD 57456
IRIDE-MS1-EAGLET 2-13
NORAD 68450
0.468 13.78 1.1e-05
2026-10-16 12:13:56 SITRO-AIS-60
NORAD 67260
IRIDE-MS1-EAGLET 2-13
NORAD 68450
1.580 12.76 1.1e-06
2026-10-16 18:44:01 IRIDE-MS1-EAGLET 2-13
NORAD 68450
SL-4 R/B
NORAD 68753
4.905 14.66 7.7e-08
2026-10-16 20:10:01 OBJECT A
NORAD 61238
IRIDE-MS1-EAGLET 2-13
NORAD 68450
4.995 6.27 1.6e-07
2026-10-16 20:57:25 OBJECT A
NORAD 61238
IRIDE-MS1-EAGLET 2-13
NORAD 68450
4.121 6.26 2.4e-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