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 26053.82632300 +.00000000 +00000-0 +68914-4 0 00002
2 22490 24.9677 193.6564 0041997 7.9742 125.3502 14.46057863 09
| Epoch (UTC): | 22 February 2026 19:49:54 |
| Eccentricity: | 0.0041997 |
| inclination: | 24.9677° |
| perigee height: | 709 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 193.6564° |
| argument of perigee: | 7.9742° |
| revolutions per day: | 14.46057863 |
| mean anomaly at epoch: | 125.3502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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