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 45567U 26145.60812347 +.00000000 +00000-0 +10169-2 0 00008
2 45567 53.0438 62.5708 0001408 65.8027 294.3132 15.59801469 03
| Epoch (UTC): | 25 May 2026 14:35:41 |
| Eccentricity: | 0.0001408 |
| inclination: | 53.0438° |
| perigee height: | 387 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 62.5708° |
| argument of perigee: | 65.8027° |
| revolutions per day: | 15.59801469 |
| mean anomaly at epoch: | 294.3132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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