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 10011U 26067.92615632 +.00000000 +00000-0 -83172-5 0 00008
2 10011 65.8632 286.5607 0692200 75.2550 14.0127 12.32267042 06
| Epoch (UTC): | 08 March 2026 22:13:39 |
| Eccentricity: | 0.0692200 |
| inclination: | 65.8632° |
| perigee height: | 991 km |
| apogee height: | 2088 km |
| right ascension of ascending node: | 286.5607° |
| argument of perigee: | 75.2550° |
| revolutions per day: | 12.32267042 |
| mean anomaly at epoch: | 14.0127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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