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 36596U 26145.62737542 +.00000000 +00000-0 +21793-3 0 00001
2 36596 97.7629 162.7881 0007134 160.4205 199.7303 15.16481187 01
| Epoch (UTC): | 25 May 2026 15:03:25 |
| Eccentricity: | 0.0007134 |
| inclination: | 97.7629° |
| perigee height: | 512 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 162.7881° |
| argument of perigee: | 160.4205° |
| revolutions per day: | 15.16481187 |
| mean anomaly at epoch: | 199.7303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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