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 45581U 26145.09873269 +.00000000 +00000-0 +12537-2 0 00008
2 45581 53.1534 79.1523 0004367 79.1092 281.0402 15.35311643 00
| Epoch (UTC): | 25 May 2026 02:22:10 |
| Eccentricity: | 0.0004367 |
| inclination: | 53.1534° |
| perigee height: | 457 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 79.1523° |
| argument of perigee: | 79.1092° |
| revolutions per day: | 15.35311643 |
| mean anomaly at epoch: | 281.0402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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