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 65791U 26145.57029345 +.00000000 +00000-0 +21452-3 0 00001
2 65791 97.4538 8.2764 0001403 91.3964 268.7424 15.05658744 01
| Epoch (UTC): | 25 May 2026 13:41:13 |
| Eccentricity: | 0.0001403 |
| inclination: | 97.4538° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 8.2764° |
| argument of perigee: | 91.3964° |
| revolutions per day: | 15.05658744 |
| mean anomaly at epoch: | 268.7424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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