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 26104.09636184 +.00000000 +00000-0 +26512-4 0 00006
2 22487 82.9453 230.0918 0036716 295.5557 237.6936 13.76035662 05
| Epoch (UTC): | 14 April 2026 02:18:45 |
| Eccentricity: | 0.0036716 |
| inclination: | 82.9453° |
| perigee height: | 951 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 230.0918° |
| argument of perigee: | 295.5557° |
| revolutions per day: | 13.76035662 |
| mean anomaly at epoch: | 237.6936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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