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 62236U 26145.34069866 +.00000000 +00000-0 +20554-3 0 00001
2 62236 53.1574 210.8329 0001106 86.0544 274.0583 15.30201850 00
| Epoch (UTC): | 25 May 2026 08:10:36 |
| Eccentricity: | 0.0001106 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.8329° |
| argument of perigee: | 86.0544° |
| revolutions per day: | 15.30201850 |
| mean anomaly at epoch: | 274.0583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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