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 26158.70270329 +.00000000 +00000-0 +94288-4 0 00008
2 00116 66.8101 274.0374 0082181 278.8963 80.2820 13.92330543 05
| Epoch (UTC): | 07 June 2026 16:51:53 |
| Eccentricity: | 0.0082181 |
| inclination: | 66.8101° |
| perigee height: | 860 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 274.0374° |
| argument of perigee: | 278.8963° |
| revolutions per day: | 13.92330543 |
| mean anomaly at epoch: | 80.2820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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