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 27845U 26098.29164604 +.00000000 +00000-0 +20884-3 0 00001
2 27845 98.6660 107.9803 0009551 52.2149 307.9894 14.24893018 04
| Epoch (UTC): | 08 April 2026 06:59:58 |
| Eccentricity: | 0.0009551 |
| inclination: | 98.6660° |
| perigee height: | 802 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 107.9803° |
| argument of perigee: | 52.2149° |
| revolutions per day: | 14.24893018 |
| mean anomaly at epoch: | 307.9894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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