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 45227U 26145.33056661 +.00000000 +00000-0 +35540-3 0 00001
2 45227 53.0650 265.7136 0001757 241.8634 118.2194 15.44340485 03
| Epoch (UTC): | 25 May 2026 07:56:00 |
| Eccentricity: | 0.0001757 |
| inclination: | 53.0650° |
| perigee height: | 432 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 265.7136° |
| argument of perigee: | 241.8634° |
| revolutions per day: | 15.44340485 |
| mean anomaly at epoch: | 118.2194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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