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 26140.75055082 +.00000000 +00000-0 +22930-3 0 00001
2 00022 50.2404 235.7332 0079040 13.4439 346.8603 15.28193274 02
| Epoch (UTC): | 20 May 2026 18:00:47 |
| Eccentricity: | 0.0079040 |
| inclination: | 50.2404° |
| perigee height: | 427 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 235.7332° |
| argument of perigee: | 13.4439° |
| revolutions per day: | 15.28193274 |
| mean anomaly at epoch: | 346.8603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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