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 68790U 26145.53154197 +.00000000 +00000-0 +15249-2 0 00009
2 68790 97.2853 182.4499 0000751 61.2184 298.9156 15.75274063 08
| Epoch (UTC): | 25 May 2026 12:45:25 |
| Eccentricity: | 0.0000751 |
| inclination: | 97.2853° |
| perigee height: | 343 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 182.4499° |
| argument of perigee: | 61.2184° |
| revolutions per day: | 15.75274063 |
| mean anomaly at epoch: | 298.9156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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