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 45625U 26145.62725412 +.00000000 +00000-0 +27485-3 0 00001
2 45625 97.5731 302.6788 0013571 142.7849 217.4332 15.25671891 09
| Epoch (UTC): | 25 May 2026 15:03:14 |
| Eccentricity: | 0.0013571 |
| inclination: | 97.5731° |
| perigee height: | 479 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 302.6788° |
| argument of perigee: | 142.7849° |
| revolutions per day: | 15.25671891 |
| mean anomaly at epoch: | 217.4332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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