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 26047.25277860 +.00000000 +00000-0 +64195-3 0 00001
2 00022 50.2477 336.9822 0083072 357.9683 2.0927 15.25936248 00
| Epoch (UTC): | 16 February 2026 06:04:00 |
| Eccentricity: | 0.0083072 |
| inclination: | 50.2477° |
| perigee height: | 431 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 336.9822° |
| argument of perigee: | 357.9683° |
| revolutions per day: | 15.25936248 |
| mean anomaly at epoch: | 2.0927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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