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 55462U 26145.64375863 +.00000000 +00000-0 +75299-5 0 00002
2 55462 43.0018 253.9059 0001264 269.3418 90.7289 15.27577946 07
| Epoch (UTC): | 25 May 2026 15:27:00 |
| Eccentricity: | 0.0001264 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 253.9059° |
| argument of perigee: | 269.3418° |
| revolutions per day: | 15.27577946 |
| mean anomaly at epoch: | 90.7289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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