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 62336U 26145.60063964 +.00000000 +00000-0 +46719-3 0 00005
2 62336 97.5244 93.3429 0002336 85.8690 274.2809 15.14094257 03
| Epoch (UTC): | 25 May 2026 14:24:55 |
| Eccentricity: | 0.0002336 |
| inclination: | 97.5244° |
| perigee height: | 522 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 93.3429° |
| argument of perigee: | 85.8690° |
| revolutions per day: | 15.14094257 |
| mean anomaly at epoch: | 274.2809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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