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 22825U 26049.75724301 +.00000000 +00000-0 +57140-4 0 00003
2 22825 98.7023 117.1490 0009524 89.0177 271.2096 14.30906361 05
| Epoch (UTC): | 18 February 2026 18:10:25 |
| Eccentricity: | 0.0009524 |
| inclination: | 98.7023° |
| perigee height: | 782 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 117.1490° |
| argument of perigee: | 89.0177° |
| revolutions per day: | 14.30906361 |
| mean anomaly at epoch: | 271.2096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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