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 26067.44245301 +.00000000 +00000-0 -88597-4 0 00000
2 23088 70.9986 73.5067 0005717 286.8109 73.2387 14.15012385 04
| Epoch (UTC): | 08 March 2026 10:37:07 |
| Eccentricity: | 0.0005717 |
| inclination: | 70.9986° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 73.5067° |
| argument of perigee: | 286.8109° |
| revolutions per day: | 14.15012385 |
| mean anomaly at epoch: | 73.2387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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