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 45721U 26145.57792406 +.00000000 +00000-0 +37214-4 0 00001
2 45721 98.4544 87.7500 0002003 190.5423 169.5720 14.34164179 01
| Epoch (UTC): | 25 May 2026 13:52:12 |
| Eccentricity: | 0.0002003 |
| inclination: | 98.4544° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 87.7500° |
| argument of perigee: | 190.5423° |
| revolutions per day: | 14.34164179 |
| mean anomaly at epoch: | 169.5720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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