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 22490U 26106.66863176 +.00000000 +00000-0 +50395-4 0 00004
2 22490 24.9687 227.4091 0041772 206.6883 176.1876 14.46092423 05
| Epoch (UTC): | 16 April 2026 16:02:49 |
| Eccentricity: | 0.0041772 |
| inclination: | 24.9687° |
| perigee height: | 709 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 227.4091° |
| argument of perigee: | 206.6883° |
| revolutions per day: | 14.46092423 |
| mean anomaly at epoch: | 176.1876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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