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ICEYE-X46

In orbit NORAD 63258 KRBX-5316-7667-5060-9809 United States of America

Observations 0
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2025

Transporter-13 Rideshare : VSFB SLC-4E

Falcon 9

Carrier rocket

База Вандерберг

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X46
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Transporter-13 Rideshare : VSFB SLC-4E
Carrier rocket
Falcon 9
Spaceport
База Вандерберг
Launch time
2025-03-15 00:00:00
Separation time
2025-03-15 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
576.39 km
Apogee
578.68 km
Inclination
97.7°
Period
96.3 min
Semi-major axis
6955.7 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 63258U 25052BA  26282.63980640  .00001900  00000-0  17624-3 0  9997
2 63258  97.6721 172.2524 0001648  82.5758 277.5650 14.95596156 85753
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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 03:16:05 ICEYE-X46
NORAD 63258 		DELTA 1 DEB
NORAD 312 		4.113 14.29 1.2e-07
2026-10-13 12:12:59 ICEYE-X46
NORAD 63258 		OBJECT L
NORAD 100965 		1.962 14.57 4.8e-07
2026-10-14 10:41:46 ICEYE-X46
NORAD 63258 		OBJECT H
NORAD 100962 		2.879 14.57 2.2e-07
2026-10-15 05:57:51 ICEYE-X46
NORAD 63258 		OBJECT G
NORAD 100961 		0.640 14.57 4.5e-06
2026-10-15 08:08:28 ICEYE-X46
NORAD 63258 		CZ-2D R/B
NORAD 36597 		3.546 14.23 1.6e-07
2026-10-15 17:12:14 ICEYE-X46
NORAD 63258 		OBJECT D
NORAD 100958 		0.365 14.57 1.4e-05
2026-10-15 18:48:36 ICEYE-X46
NORAD 63258 		OBJECT F
NORAD 100960 		4.958 14.57 7.5e-08
2026-10-16 10:52:01 ICEYE-X46
NORAD 63258 		OBJECT C
NORAD 100957 		3.832 14.57 1.2e-07
2026-10-16 12:28:20 ICEYE-X46
NORAD 63258 		OBJECT B
NORAD 100956 		1.025 14.57 1.7e-06
2026-10-16 20:30:03 ICEYE-X46
NORAD 63258 		OBJECT A
NORAD 100955 		2.461 14.57 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