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

IRIDE-MS1-EAGLET 2-13

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

Observations 0
Go to map
Back

—

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 2-13
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
500.68 km
Apogee
503.96 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6880.5 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68450U 26067AL  26286.86239112  .00007539  00000-0  35143-3 0  9993
2 68450  97.4701 243.9603 0002382  21.8867 338.2469 15.20161657 29962
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
2026-10-15 09:16:33 IRIDE-MS1-EAGLET 2-13
NORAD 68450 		COSMOS 252 DEB
NORAD 19479 		3.909 14.52 1.3e-07
2026-10-16 22:32:10 OBJECT A
NORAD 61238 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		0.887 6.26 5.2e-06
2026-10-17 07:11:21 PIAST-S2
NORAD 66757 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		4.027 12.72 1.7e-07
2026-10-18 00:34:29 GAOFEN-7
NORAD 44703 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		4.543 11.90 1.4e-07
2026-10-19 02:38:01 OBJECT E
NORAD 61231 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		3.791 12.54 1.9e-07
2026-10-19 03:25:25 OBJECT E
NORAD 61231 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		4.165 12.57 1.6e-07
2026-10-19 09:02:54 IRIDE-MS1-EAGLET 2-13
NORAD 68450 		ELECTRON KICK STAGE R/B
NORAD 45728 		2.697 12.31 3.9e-07
2026-10-19 16:04:13 MONITOR-2 (RS39S)
NORAD 57184 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		3.494 11.60 2.5e-07
2026-10-19 19:49:05 SPACEMOBILE-003
NORAD 61045 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		1.183 14.37 1.4e-06
2026-10-20 03:01:28 CONNECTA IOT-10
NORAD 64555 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		3.922 14.79 1.2e-07
2026-10-20 03:48:51 CONNECTA IOT-10
NORAD 64555 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		4.418 14.76 9.1e-08
2026-10-20 17:47:24 BLACKJACK ACES-3
NORAD 56950 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		4.561 15.08 7.5e-08
2026-10-20 19:22:13 BLACKJACK ACES-3
NORAD 56950 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		0.954 15.08 1.7e-06
2026-10-20 20:57:01 BLACKJACK ACES-3
NORAD 56950 		IRIDE-MS1-EAGLET 2-13
NORAD 68450 		4.279 15.08 8.6e-08

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