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 62333U 26145.61802948 +.00000000 +00000-0 +39574-3 0 00007
2 62333 97.5311 93.5267 0002289 87.2445 272.9048 15.14073586 00
| Epoch (UTC): | 25 May 2026 14:49:57 |
| Eccentricity: | 0.0002289 |
| inclination: | 97.5311° |
| perigee height: | 522 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 93.5267° |
| argument of perigee: | 87.2445° |
| revolutions per day: | 15.14073586 |
| mean anomaly at epoch: | 272.9048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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