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 26108.61395368 +.00000000 +00000-0 +31879-4 0 00009
2 27386 98.3790 61.2773 0001152 85.1240 88.3750 14.39050090 01
| Epoch (UTC): | 18 April 2026 14:44:05 |
| Eccentricity: | 0.0001152 |
| inclination: | 98.3790° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 61.2773° |
| argument of perigee: | 85.1240° |
| revolutions per day: | 14.39050090 |
| mean anomaly at epoch: | 88.3750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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