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 26049.87216455 +.00000000 +00000-0 +46109-3 0 00009
2 00022 50.2467 324.0871 0082889 8.5460 351.6889 15.26017314 03
| Epoch (UTC): | 18 February 2026 20:55:55 |
| Eccentricity: | 0.0082889 |
| inclination: | 50.2467° |
| perigee height: | 431 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 324.0871° |
| argument of perigee: | 8.5460° |
| revolutions per day: | 15.26017314 |
| mean anomaly at epoch: | 351.6889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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