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 22487U 26160.21063529 +.00000000 +00000-0 +36953-4 0 00009
2 22487 82.9441 188.4776 0039060 136.4176 295.3482 13.76040582 09
| Epoch (UTC): | 09 June 2026 05:03:18 |
| Eccentricity: | 0.0039060 |
| inclination: | 82.9441° |
| perigee height: | 949 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 188.4776° |
| argument of perigee: | 136.4176° |
| revolutions per day: | 13.76040582 |
| mean anomaly at epoch: | 295.3482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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