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 27540U 26132.16299502 +.00000000 +00000-0 +00000-0 0 00009
2 27540 90.1707 349.0037 8686596 261.3877 349.6577 0.37580049 09
| Epoch (UTC): | 12 May 2026 03:54:42 |
| Eccentricity: | 0.8686596 |
| inclination: | 90.1707° |
| perigee height: | 4275 km |
| apogee height: | 145197 km |
| right ascension of ascending node: | 349.0037° |
| argument of perigee: | 261.3877° |
| revolutions per day: | 0.37580049 |
| mean anomaly at epoch: | 349.6577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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