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 26133.27411022 +.00000000 +00000-0 +40329-4 0 00007
2 00116 66.8102 336.2630 0081547 295.3859 63.8795 13.92325808 01
| Epoch (UTC): | 13 May 2026 06:34:43 |
| Eccentricity: | 0.0081547 |
| inclination: | 66.8102° |
| perigee height: | 861 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 336.2630° |
| argument of perigee: | 295.3859° |
| revolutions per day: | 13.92325808 |
| mean anomaly at epoch: | 63.8795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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