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 53000U 26145.19666966 +.00000000 +00000-0 +28430-4 0 00009
2 53000 53.2134 110.6672 0001399 76.6665 283.4483 15.08835174 03
| Epoch (UTC): | 25 May 2026 04:43:12 |
| Eccentricity: | 0.0001399 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.6672° |
| argument of perigee: | 76.6665° |
| revolutions per day: | 15.08835174 |
| mean anomaly at epoch: | 283.4483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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