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 00022U 26049.21733096 +.00000000 +00000-0 +52795-3 0 00000
2 00022 50.2471 327.3108 0082918 5.8989 354.2928 15.25999935 06
| Epoch (UTC): | 18 February 2026 05:12:57 |
| Eccentricity: | 0.0082918 |
| inclination: | 50.2471° |
| perigee height: | 431 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 327.3108° |
| argument of perigee: | 5.8989° |
| revolutions per day: | 15.25999935 |
| mean anomaly at epoch: | 354.2928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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