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 26073.86861888 +.00000000 +00000-0 +66121-4 0 00002
2 00116 66.8082 121.6264 0078329 334.5231 25.1995 13.92313533 06
| Epoch (UTC): | 14 March 2026 20:50:48 |
| Eccentricity: | 0.0078329 |
| inclination: | 66.8082° |
| perigee height: | 863 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 121.6264° |
| argument of perigee: | 334.5231° |
| revolutions per day: | 13.92313533 |
| mean anomaly at epoch: | 25.1995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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