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 26049.58908279 +.00000000 +00000-0 +81975-4 0 00004
2 00116 66.8091 181.0325 0076278 351.2043 8.7694 13.92308300 01
| Epoch (UTC): | 18 February 2026 14:08:16 |
| Eccentricity: | 0.0076278 |
| inclination: | 66.8091° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 181.0325° |
| argument of perigee: | 351.2043° |
| revolutions per day: | 13.92308300 |
| mean anomaly at epoch: | 8.7694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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