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 26048.23506522 +.00000000 +00000-0 +62020-3 0 00005
2 00022 50.2475 332.1465 0082981 1.9264 358.2000 15.25970414 09
| Epoch (UTC): | 17 February 2026 05:38:29 |
| Eccentricity: | 0.0082981 |
| inclination: | 50.2475° |
| perigee height: | 431 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 332.1465° |
| argument of perigee: | 1.9264° |
| revolutions per day: | 15.25970414 |
| mean anomaly at epoch: | 358.2000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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