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 45540U 26145.61165154 +.00000000 +00000-0 +12138-2 0 00005
2 45540 53.1569 102.6675 0004831 73.9639 286.1896 15.35938513 02
| Epoch (UTC): | 25 May 2026 14:40:46 |
| Eccentricity: | 0.0004831 |
| inclination: | 53.1569° |
| perigee height: | 455 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 102.6675° |
| argument of perigee: | 73.9639° |
| revolutions per day: | 15.35938513 |
| mean anomaly at epoch: | 286.1896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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