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 63166U 26145.56115870 +.00000000 +00000-0 +37419-4 0 00004
2 63166 88.9691 302.8229 0014137 27.3864 332.8030 13.51005291 03
| Epoch (UTC): | 25 May 2026 13:28:04 |
| Eccentricity: | 0.0014137 |
| inclination: | 88.9691° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 302.8229° |
| argument of perigee: | 27.3864° |
| revolutions per day: | 13.51005291 |
| mean anomaly at epoch: | 332.8030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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