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 53807U 26074.52245215 +.00000000 +00000-0 +16120-3 0 00004
2 53807 53.2289 113.3356 0004522 247.5098 112.5428 15.37222138 01
| Epoch (UTC): | 15 March 2026 12:32:19 |
| Eccentricity: | 0.0004522 |
| inclination: | 53.2289° |
| perigee height: | 451 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 113.3356° |
| argument of perigee: | 247.5098° |
| revolutions per day: | 15.37222138 |
| mean anomaly at epoch: | 112.5428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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