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 26022.07694878 +.00000000 +00000-0 +14830-3 0 00001
2 00116 66.8079 248.3513 0073968 10.5440 349.7169 13.92301427 00
| Epoch (UTC): | 22 January 2026 01:50:48 |
| Eccentricity: | 0.0073968 |
| inclination: | 66.8079° |
| perigee height: | 867 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 248.3513° |
| argument of perigee: | 10.5440° |
| revolutions per day: | 13.92301427 |
| mean anomaly at epoch: | 349.7169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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