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 26070.27012793 +.00000000 +00000-0 -97399-4 0 00002
2 23088 70.9986 67.5677 0005699 284.0299 76.0190 14.15011278 06
| Epoch (UTC): | 11 March 2026 06:28:59 |
| Eccentricity: | 0.0005699 |
| inclination: | 70.9986° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 67.5677° |
| argument of perigee: | 284.0299° |
| revolutions per day: | 14.15011278 |
| mean anomaly at epoch: | 76.0190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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