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 65595U 26145.44055213 +.00000000 +00000-0 +27146-3 0 00008
2 65595 97.4502 213.9954 0001080 173.0913 187.0329 15.05653142 07
| Epoch (UTC): | 25 May 2026 10:34:23 |
| Eccentricity: | 0.0001080 |
| inclination: | 97.4502° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 213.9954° |
| argument of perigee: | 173.0913° |
| revolutions per day: | 15.05653142 |
| mean anomaly at epoch: | 187.0329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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