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 26041.35858726 +.00000000 +00000-0 +64287-3 0 00004
2 00022 50.2472 5.9944 0083573 334.2065 25.4739 15.25720553 01
| Epoch (UTC): | 10 February 2026 08:36:21 |
| Eccentricity: | 0.0083573 |
| inclination: | 50.2472° |
| perigee height: | 431 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 5.9944° |
| argument of perigee: | 334.2065° |
| revolutions per day: | 15.25720553 |
| mean anomaly at epoch: | 25.4739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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