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 52618U 26145.38849437 +.00000000 +00000-0 +11352-3 0 00004
2 52618 53.2147 284.8057 0001412 85.8078 274.3075 15.08841301 03
| Epoch (UTC): | 25 May 2026 09:19:25 |
| Eccentricity: | 0.0001412 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.8057° |
| argument of perigee: | 85.8078° |
| revolutions per day: | 15.08841301 |
| mean anomaly at epoch: | 274.3075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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