View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 55460U 26145.34124049 +.00000000 +00000-0 +21416-4 0 00006
2 55460 43.0029 255.9427 0001361 268.3198 91.7498 15.27576595 02
| Epoch (UTC): | 25 May 2026 08:11:23 |
| Eccentricity: | 0.0001361 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 255.9427° |
| argument of perigee: | 268.3198° |
| revolutions per day: | 15.27576595 |
| mean anomaly at epoch: | 91.7498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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