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 69045U 26145.57892132 +.00000000 +00000-0 +10149-2 0 00009
2 69045 97.2849 0.3840 0001323 72.5308 287.6102 15.75223963 03
| Epoch (UTC): | 25 May 2026 13:53:38 |
| Eccentricity: | 0.0001323 |
| inclination: | 97.2849° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 0.3840° |
| argument of perigee: | 72.5308° |
| revolutions per day: | 15.75223963 |
| mean anomaly at epoch: | 287.6102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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