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 27844U 26137.47907676 +.00000000 +00000-0 +95961-4 0 00007
2 27844 98.6745 146.4240 0008283 275.4174 84.6060 14.24315278 09
| Epoch (UTC): | 17 May 2026 11:29:52 |
| Eccentricity: | 0.0008283 |
| inclination: | 98.6745° |
| perigee height: | 805 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 146.4240° |
| argument of perigee: | 275.4174° |
| revolutions per day: | 14.24315278 |
| mean anomaly at epoch: | 84.6060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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