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 26069.42182521 +.00000000 +00000-0 -98609-4 0 00009
2 23088 70.9986 69.3494 0005711 284.9255 75.1235 14.15011602 00
| Epoch (UTC): | 10 March 2026 10:07:25 |
| Eccentricity: | 0.0005711 |
| inclination: | 70.9986° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 69.3494° |
| argument of perigee: | 284.9255° |
| revolutions per day: | 14.15011602 |
| mean anomaly at epoch: | 75.1235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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