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 62235U 26145.55360830 +.00000000 +00000-0 +30035-3 0 00003
2 62235 53.1593 209.3258 0001048 72.0190 288.0926 15.31711183 03
| Epoch (UTC): | 25 May 2026 13:17:11 |
| Eccentricity: | 0.0001048 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.3258° |
| argument of perigee: | 72.0190° |
| revolutions per day: | 15.31711183 |
| mean anomaly at epoch: | 288.0926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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