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 26040.89727365 +.00000000 +00000-0 +88619-4 0 00006
2 00116 66.8079 202.2993 0075563 357.2775 2.7883 13.92306281 08
| Epoch (UTC): | 09 February 2026 21:32:04 |
| Eccentricity: | 0.0075563 |
| inclination: | 66.8079° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 202.2993° |
| argument of perigee: | 357.2775° |
| revolutions per day: | 13.92306281 |
| mean anomaly at epoch: | 2.7883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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