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 23088U 26065.32169851 +.00000000 +00000-0 -68676-4 0 00006
2 23088 70.9986 77.9609 0005695 288.8916 71.1589 14.15012986 05
| Epoch (UTC): | 06 March 2026 07:43:14 |
| Eccentricity: | 0.0005695 |
| inclination: | 70.9986° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 77.9609° |
| argument of perigee: | 288.8916° |
| revolutions per day: | 14.15012986 |
| mean anomaly at epoch: | 71.1589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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