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 65808U 26145.60630043 +.00000000 +00000-0 +28357-3 0 00008
2 65808 97.4509 8.3836 0002795 85.4236 274.7310 15.05659567 05
| Epoch (UTC): | 25 May 2026 14:33:04 |
| Eccentricity: | 0.0002795 |
| inclination: | 97.4509° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.3836° |
| argument of perigee: | 85.4236° |
| revolutions per day: | 15.05659567 |
| mean anomaly at epoch: | 274.7310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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