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 26037.80844587 +.00000000 +00000-0 +80449-4 0 00002
2 00116 66.8075 209.8576 0075311 359.4447 0.6536 13.92305626 09
| Epoch (UTC): | 06 February 2026 19:24:09 |
| Eccentricity: | 0.0075311 |
| inclination: | 66.8075° |
| perigee height: | 866 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 209.8576° |
| argument of perigee: | 359.4447° |
| revolutions per day: | 13.92305626 |
| mean anomaly at epoch: | 0.6536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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