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 27168U 26145.30234977 +.00000000 +00000-0 +00000-0 0 00000
2 27168 11.1534 22.0518 0100045 7.5285 341.1142 1.00268843 04
| Epoch (UTC): | 25 May 2026 07:15:23 |
| Eccentricity: | 0.0100045 |
| inclination: | 11.1534° |
| perigee height: | 35366 km |
| apogee height: | 36209 km |
| right ascension of ascending node: | 22.0518° |
| argument of perigee: | 7.5285° |
| revolutions per day: | 1.00268843 |
| mean anomaly at epoch: | 341.1142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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