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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
500.59 km
Apogee
502.74 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6879.8 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68447U 26067AH  26287.10565437  .00008612  00000-0  39845-3 0  9995
2 68447  97.4672 244.1739 0001562  39.2491 320.8858 15.20378887 30004
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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
2026-10-15 16:01:30 IRIDE-MS1-EAGLET 2-14
NORAD 68447 		RASSVET-3 29
NORAD 100095 		4.812 12.44 1.2e-07
2026-10-16 08:58:15 OBJECT A
NORAD 63291 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.607 15.09 7.4e-08
2026-10-16 14:54:21 TIANYI D
NORAD 64051 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		1.982 12.47 7.1e-07
2026-10-16 15:41:44 TIANYI D
NORAD 64051 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		3.370 12.44 2.5e-07
2026-10-16 23:14:22 RASSVET-3 8
NORAD 68367 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.354 2.01 2.3e-07
2026-10-17 07:21:55 STARLINK-5862
NORAD 55920 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.546 14.96 2.4e-06
2026-10-17 08:09:18 STARLINK-5862
NORAD 55920 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		2.934 14.98 5.8e-06
2026-10-17 19:24:45 STARLINK-4440
NORAD 53671 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		3.763 10.16 7.3e-06
2026-10-19 21:09:33 TRANSPORTER-13 OBJECT M
NORAD 63221 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.732 8.33 1.7e-07
2026-10-20 10:25:59 SUPERVIEW NEO-1 03
NORAD 63125 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.158 14.73 1.0e-07
2026-10-20 12:48:06 SUPERVIEW NEO-1 03
NORAD 63125 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		4.265 14.70 1.0e-07
2026-10-21 01:06:00 YAOGAN-36 02A
NORAD 54042 		IRIDE-MS1-EAGLET 2-14
NORAD 68447 		3.732 13.75 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