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 26133.81905249 +.00000000 +00000-0 +17918-3 0 00009
2 00022 50.2430 269.9733 0079299 345.6160 14.2544 15.28113399 02
| Epoch (UTC): | 13 May 2026 19:39:26 |
| Eccentricity: | 0.0079299 |
| inclination: | 50.2430° |
| perigee height: | 427 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 269.9733° |
| argument of perigee: | 345.6160° |
| revolutions per day: | 15.28113399 |
| mean anomaly at epoch: | 14.2544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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