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 69047U 26145.57503941 +.00000000 +00000-0 +94174-3 0 00009
2 69047 97.2849 0.3905 0001246 77.3626 282.7779 15.75217901 08
| Epoch (UTC): | 25 May 2026 13:48:03 |
| Eccentricity: | 0.0001246 |
| inclination: | 97.2849° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 0.3905° |
| argument of perigee: | 77.3626° |
| revolutions per day: | 15.75217901 |
| mean anomaly at epoch: | 282.7779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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