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 45024U 26145.60797926 +.00000000 +00000-0 +59394-4 0 00006
2 45024 86.3922 125.6831 0015990 80.3612 279.9414 14.79101375 01
| Epoch (UTC): | 25 May 2026 14:35:29 |
| Eccentricity: | 0.0015990 |
| inclination: | 86.3922° |
| perigee height: | 621 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 125.6831° |
| argument of perigee: | 80.3612° |
| revolutions per day: | 14.79101375 |
| mean anomaly at epoch: | 279.9414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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