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IRIDE-MS1-EAGLET 2-14

In orbit NORAD 68447 DVDJ-8341-9800-8763-6193

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 2-14
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
500.52 km
Apogee
503.18 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6880.0 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:59 UTC
Two-line elements (TLE)
1 68447U 26067AH  26283.61739257  .00007398  00000-0  34341-3 0  9996
2 68447  97.4658 240.7199 0001936  42.9262 317.2124 15.20317311 29472
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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
2026-10-11 12:02:36 RASSVET-3 10
NORAD 68369 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.197 2.17 2.5e-07
2026-10-11 12:31:29 CONNECTA IOT-15
NORAD 67402 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.174 5.17 2.4e-07
2026-10-11 16:28:38 IRIDE-MS1-EAGLET 2-14
NORAD 68447 		SL-3 R/B
NORAD 19046 		3.853 3.39 8.0e-07
2026-10-11 17:13:41 OBJECT B
NORAD 66054 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.721 12.43 1.3e-07
2026-10-13 10:59:40 ION SCV-020
NORAD 64545 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		2.869 14.79 2.2e-07
2026-10-13 12:34:27 ION SCV-020
NORAD 64545 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.325 14.79 9.5e-08
2026-10-13 23:21:03 QPS-SAR-5 (TSUKUYOMI-I)
NORAD 58578 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		2.756 14.26 2.7e-07
2026-10-14 05:15:10 TIANYI F
NORAD 64053 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.700 12.46 1.3e-07
2026-10-14 06:02:34 TIANYI F
NORAD 64053 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		0.327 12.49 2.6e-05
2026-10-14 20:22:34 OBJECT B
NORAD 49316 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		3.345 13.75 2.1e-07
2026-10-16 14:06:39 MBZ-SAT
NORAD 62626 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.804 12.94 1.1e-07
2026-10-16 18:03:59 TIANYI D
NORAD 64051 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		2.650 12.47 4.0e-07
2026-10-16 18:51:23 TIANYI D
NORAD 64051 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		2.482 12.44 4.6e-07
2026-10-17 01:10:24 IRIDE-MS1-EAGLET 2-14
NORAD 68447 		OBJECT B
NORAD 100367 		3.031 12.49 3.0e-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