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 00116U 26102.24252742 +.00000000 +00000-0 +87327-4 0 00001
2 00116 66.8102 52.1935 0080264 315.6455 43.8212 13.92320424 07
| Epoch (UTC): | 12 April 2026 05:49:14 |
| Eccentricity: | 0.0080264 |
| inclination: | 66.8102° |
| perigee height: | 862 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 52.1935° |
| argument of perigee: | 315.6455° |
| revolutions per day: | 13.92320424 |
| mean anomaly at epoch: | 43.8212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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