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 26071.53167866 +.00000000 +00000-0 +15522-3 0 00002
2 53807 53.2292 127.3533 0004621 235.8196 124.2371 15.37190908 02
| Epoch (UTC): | 12 March 2026 12:45:37 |
| Eccentricity: | 0.0004621 |
| inclination: | 53.2292° |
| perigee height: | 451 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 127.3533° |
| argument of perigee: | 235.8196° |
| revolutions per day: | 15.37190908 |
| mean anomaly at epoch: | 124.2371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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