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 26106.47566500 +.00000000 +00000-0 +17732-4 0 00008
2 22487 82.9456 228.3270 0036657 288.6632 144.3588 13.76035814 06
| Epoch (UTC): | 16 April 2026 11:24:57 |
| Eccentricity: | 0.0036657 |
| inclination: | 82.9456° |
| perigee height: | 951 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 228.3270° |
| argument of perigee: | 288.6632° |
| revolutions per day: | 13.76035814 |
| mean anomaly at epoch: | 144.3588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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