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 53863U 26145.41101311 +.00000000 +00000-0 -97998-3 0 00004
2 53863 53.2133 299.7424 0001448 67.9516 292.1630 15.08912034 08
| Epoch (UTC): | 25 May 2026 09:51:51 |
| Eccentricity: | 0.0001448 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.7424° |
| argument of perigee: | 67.9516° |
| revolutions per day: | 15.08912034 |
| mean anomaly at epoch: | 292.1630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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