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 27386U 26158.31801014 +.00000000 +00000-0 +52019-4 0 00000
2 27386 98.3831 109.8569 0001342 91.0289 30.3146 14.39062585 07
| Epoch (UTC): | 07 June 2026 07:37:56 |
| Eccentricity: | 0.0001342 |
| inclination: | 98.3831° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 109.8569° |
| argument of perigee: | 91.0289° |
| revolutions per day: | 14.39062585 |
| mean anomaly at epoch: | 30.3146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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