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 69022U 26145.45880156 +.00000000 +00000-0 +27294-3 0 00004
2 69022 97.4050 43.6602 0006900 76.6841 283.5163 15.19635571 05
| Epoch (UTC): | 25 May 2026 11:00:40 |
| Eccentricity: | 0.0006900 |
| inclination: | 97.4050° |
| perigee height: | 502 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 43.6602° |
| argument of perigee: | 76.6841° |
| revolutions per day: | 15.19635571 |
| mean anomaly at epoch: | 283.5163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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