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 26046.13949365 +.00000000 +00000-0 +54674-3 0 00004
2 00022 50.2477 342.4631 0083199 353.4782 6.5088 15.25892644 09
| Epoch (UTC): | 15 February 2026 03:20:52 |
| Eccentricity: | 0.0083199 |
| inclination: | 50.2477° |
| perigee height: | 431 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 342.4631° |
| argument of perigee: | 353.4782° |
| revolutions per day: | 15.25892644 |
| mean anomaly at epoch: | 6.5088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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