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 26145.87260024 +.00000000 +00000-0 +00000-0 0 00004
2 27168 11.1540 22.0482 0100054 7.5700 186.9217 1.00269140 02
| Epoch (UTC): | 25 May 2026 20:56:32 |
| Eccentricity: | 0.0100054 |
| inclination: | 11.1540° |
| perigee height: | 35365 km |
| apogee height: | 36209 km |
| right ascension of ascending node: | 22.0482° |
| argument of perigee: | 7.5700° |
| revolutions per day: | 1.00269140 |
| mean anomaly at epoch: | 186.9217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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