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 45425U 26145.37195370 +.00000000 +00000-0 -55562-3 0 00003
2 45425 87.8929 25.5284 0001979 84.6790 275.4563 13.11421146 07
| Epoch (UTC): | 25 May 2026 08:55:36 |
| Eccentricity: | 0.0001979 |
| inclination: | 87.8929° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5284° |
| argument of perigee: | 84.6790° |
| revolutions per day: | 13.11421146 |
| mean anomaly at epoch: | 275.4563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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