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 26048.87075188 +.00000000 +00000-0 +77727-4 0 00009
2 00116 66.8090 182.7900 0076221 351.7054 8.2759 13.92308134 04
| Epoch (UTC): | 17 February 2026 20:53:52 |
| Eccentricity: | 0.0076221 |
| inclination: | 66.8090° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 182.7900° |
| argument of perigee: | 351.7054° |
| revolutions per day: | 13.92308134 |
| mean anomaly at epoch: | 8.2759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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