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 45569U 26145.05040676 +.00000000 +00000-0 +63249-3 0 00005
2 45569 53.0326 11.3848 0004281 256.5302 103.5252 16.02263127 01
| Epoch (UTC): | 25 May 2026 01:12:35 |
| Eccentricity: | 0.0004281 |
| inclination: | 53.0326° |
| perigee height: | 265 km |
| apogee height: | 271 km |
| right ascension of ascending node: | 11.3848° |
| argument of perigee: | 256.5302° |
| revolutions per day: | 16.02263127 |
| mean anomaly at epoch: | 103.5252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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