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 26048.88991140 +.00000000 +00000-0 +51304-3 0 00003
2 00022 50.2472 328.9228 0082963 4.5779 355.5921 15.25988864 06
| Epoch (UTC): | 17 February 2026 21:21:28 |
| Eccentricity: | 0.0082963 |
| inclination: | 50.2472° |
| perigee height: | 431 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 328.9228° |
| argument of perigee: | 4.5779° |
| revolutions per day: | 15.25988864 |
| mean anomaly at epoch: | 355.5921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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