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 69073U 26145.32241097 +.00000000 +00000-0 +32989-4 0 00009
2 69073 88.9868 344.2299 0004496 170.9380 189.1894 14.23183324 09
| Epoch (UTC): | 25 May 2026 07:44:16 |
| Eccentricity: | 0.0004496 |
| inclination: | 88.9868° |
| perigee height: | 811 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 344.2299° |
| argument of perigee: | 170.9380° |
| revolutions per day: | 14.23183324 |
| mean anomaly at epoch: | 189.1894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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