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 26109.22819127 +.00000000 +00000-0 +26694-3 0 00007
2 00022 50.2458 31.4033 0079429 246.7672 112.4910 15.27695596 02
| Epoch (UTC): | 19 April 2026 05:28:35 |
| Eccentricity: | 0.0079429 |
| inclination: | 50.2458° |
| perigee height: | 428 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 31.4033° |
| argument of perigee: | 246.7672° |
| revolutions per day: | 15.27695596 |
| mean anomaly at epoch: | 112.4910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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