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 26071.18172530 +.00000000 +00000-0 +33928-3 0 00003
2 36596 97.7700 86.6102 0008403 75.4042 284.8121 15.15745700 02
| Epoch (UTC): | 12 March 2026 04:21:41 |
| Eccentricity: | 0.0008403 |
| inclination: | 97.7700° |
| perigee height: | 513 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 86.6102° |
| argument of perigee: | 75.4042° |
| revolutions per day: | 15.15745700 |
| mean anomaly at epoch: | 284.8121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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