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 45755U 26145.37123867 +.00000000 +00000-0 +44557-3 0 00002
2 45755 53.0451 183.4833 0004551 26.8227 333.3022 15.66692205 06
| Epoch (UTC): | 25 May 2026 08:54:35 |
| Eccentricity: | 0.0004551 |
| inclination: | 53.0451° |
| perigee height: | 365 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 183.4833° |
| argument of perigee: | 26.8227° |
| revolutions per day: | 15.66692205 |
| mean anomaly at epoch: | 333.3022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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