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 27663U 26145.26291218 +.00000000 +00000-0 +00000-0 0 00006
2 27663 54.8858 215.8797 0147949 53.0214 14.4311 2.00561815 04
| Epoch (UTC): | 25 May 2026 06:18:35 |
| Eccentricity: | 0.0147949 |
| inclination: | 54.8858° |
| perigee height: | 19789 km |
| apogee height: | 20575 km |
| right ascension of ascending node: | 215.8797° |
| argument of perigee: | 53.0214° |
| revolutions per day: | 2.00561815 |
| mean anomaly at epoch: | 14.4311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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