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 53813U 26145.52857178 +.00000000 +00000-0 +00000-0 0 00004
2 53813 0.0116 297.6234 0000843 55.1726 162.0094 1.00270415 06
| Epoch (UTC): | 25 May 2026 12:41:08 |
| Eccentricity: | 0.0000843 |
| inclination: | 0.0116° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 297.6234° |
| argument of perigee: | 55.1726° |
| revolutions per day: | 1.00270415 |
| mean anomaly at epoch: | 162.0094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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