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 27846U 26103.71237096 +.00000000 +00000-0 +90707-4 0 00004
2 27846 98.6875 112.9661 0009065 357.3583 2.7547 14.23929397 06
| Epoch (UTC): | 13 April 2026 17:05:48 |
| Eccentricity: | 0.0009065 |
| inclination: | 98.6875° |
| perigee height: | 806 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 112.9661° |
| argument of perigee: | 357.3583° |
| revolutions per day: | 14.23929397 |
| mean anomaly at epoch: | 2.7547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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