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 26088.12908801 +.00000000 +00000-0 +96928-4 0 00001
2 22490 24.9707 341.8747 0041919 10.9961 140.3672 14.46080001 09
| Epoch (UTC): | 29 March 2026 03:05:53 |
| Eccentricity: | 0.0041919 |
| inclination: | 24.9707° |
| perigee height: | 709 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 341.8747° |
| argument of perigee: | 10.9961° |
| revolutions per day: | 14.46080001 |
| mean anomaly at epoch: | 140.3672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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