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 52422U 26145.60325824 +.00000000 +00000-0 +36458-3 0 00005
2 52422 97.3402 236.2519 0005713 147.5345 212.6258 15.49036940 02
| Epoch (UTC): | 25 May 2026 14:28:41 |
| Eccentricity: | 0.0005713 |
| inclination: | 97.3402° |
| perigee height: | 416 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 236.2519° |
| argument of perigee: | 147.5345° |
| revolutions per day: | 15.49036940 |
| mean anomaly at epoch: | 212.6258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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