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 26138.81454147 +.00000000 +00000-0 +00000-0 0 00001
2 27168 11.1458 22.0883 0099388 7.5555 159.1112 1.00276913 02
| Epoch (UTC): | 18 May 2026 19:32:56 |
| Eccentricity: | 0.0099388 |
| inclination: | 11.1458° |
| perigee height: | 35366 km |
| apogee height: | 36204 km |
| right ascension of ascending node: | 22.0883° |
| argument of perigee: | 7.5555° |
| revolutions per day: | 1.00276913 |
| mean anomaly at epoch: | 159.1112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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