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 36605U 26150.40728882 +.00000000 +00000-0 +62040-4 0 00002
2 36605 97.4447 158.3676 0001781 81.6936 278.4501 15.19152610 01
| Epoch (UTC): | 30 May 2026 09:46:29 |
| Eccentricity: | 0.0001781 |
| inclination: | 97.4447° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 158.3676° |
| argument of perigee: | 81.6936° |
| revolutions per day: | 15.19152610 |
| mean anomaly at epoch: | 278.4501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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