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 02180U 26100.22388904 +.00000000 +00000-0 +22058-3 0 00009
2 02180 90.2201 80.8522 0078184 174.3748 185.8329 14.01084586 07
| Epoch (UTC): | 10 April 2026 05:22:24 |
| Eccentricity: | 0.0078184 |
| inclination: | 90.2201° |
| perigee height: | 833 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 80.8522° |
| argument of perigee: | 174.3748° |
| revolutions per day: | 14.01084586 |
| mean anomaly at epoch: | 185.8329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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