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 45727U 26145.50215699 +.00000000 +00000-0 +10130-3 0 00001
2 45727 97.8149 336.4804 0010397 224.6608 135.3781 15.04554148 06
| Epoch (UTC): | 25 May 2026 12:03:06 |
| Eccentricity: | 0.0010397 |
| inclination: | 97.8149° |
| perigee height: | 546 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 336.4804° |
| argument of perigee: | 224.6608° |
| revolutions per day: | 15.04554148 |
| mean anomaly at epoch: | 135.3781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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