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 62233U 26145.44177815 +.00000000 +00000-0 +48322-3 0 00006
2 62233 53.1598 210.0445 0000367 100.8403 259.2640 15.31710104 08
| Epoch (UTC): | 25 May 2026 10:36:09 |
| Eccentricity: | 0.0000367 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 210.0445° |
| argument of perigee: | 100.8403° |
| revolutions per day: | 15.31710104 |
| mean anomaly at epoch: | 259.2640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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