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 53418U 26145.61889752 +.00000000 +00000-0 +38955-4 0 00002
2 53418 53.2129 118.3349 0001197 73.8135 286.2988 15.08832814 02
| Epoch (UTC): | 25 May 2026 14:51:12 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 118.3349° |
| argument of perigee: | 73.8135° |
| revolutions per day: | 15.08832814 |
| mean anomaly at epoch: | 286.2988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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