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IRIDE-MS1-EAGLET 2-9

In orbit NORAD 68449 ZYJP-5534-4146-2259-7915

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 2-9
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
501.17 km
Apogee
508.59 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6882.9 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:42 UTC
Two-line elements (TLE)
1 68449U 26067AK  26285.31466001  .00007221  00000-0  34471-3 0  9990
2 68449  97.4660 242.1100 0005262  41.1979 318.9652 15.19345102 29715
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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 13:43:30 RASSVET-3 9
NORAD 68368 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		3.981 2.41 2.8e-07
2026-10-13 09:11:11 FLOCK 4H-32
NORAD 66735 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		3.590 12.72 2.1e-07
2026-10-13 18:25:31 IRIDE-MS1-EAGLET 2-9
NORAD 68449 		HULIANWANG JISHU SHIYAN 9B
NORAD 68832 		3.521 6.01 3.3e-07
2026-10-13 21:52:43 IRIDE-MS1-EAGLET 2-9
NORAD 68449 		TRANSPORTER-16 OBJECT AT
NORAD 68457 		4.650 0.07 2.0e-07
2026-10-14 02:35:09 OBJECT P
NORAD 57179 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		2.144 11.40 6.8e-07
2026-10-14 04:56:19 LEGION 1
NORAD 59625 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		0.935 13.03 3.0e-06
2026-10-14 13:04:24 AAC-HSI-SAT2
NORAD 56995 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		3.259 14.87 1.6e-07
2026-10-16 15:26:45 IRIDE-MS1-EAGLET 2-9
NORAD 68449 		OBJECT BA
NORAD 43806 		4.908 10.42 1.4e-07
2026-10-16 22:31:54 CAS-2T & KS-1Q
NORAD 41847 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		4.592 13.00 1.3e-07
2026-10-17 02:05:11 RASSVET-3 12
NORAD 68371 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		0.339 2.06 3.8e-05
2026-10-17 12:54:44 DB-WALI-WMU
NORAD 68443 		IRIDE-MS1-EAGLET 2-9
NORAD 68449 		3.547 0.01 3.4e-07
2026-10-18 02:36:29 IRIDE-MS1-EAGLET 2-9
NORAD 68449 		FREGAT DEB
NORAD 45638 		3.710 14.95 1.4e-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