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 62396U 26145.06276638 +.00000000 +00000-0 +70466-3 0 00001
2 62396 44.9946 20.5549 0007619 173.4052 186.6941 15.50495558 06
| Epoch (UTC): | 25 May 2026 01:30:23 |
| Eccentricity: | 0.0007619 |
| inclination: | 44.9946° |
| perigee height: | 410 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 20.5549° |
| argument of perigee: | 173.4052° |
| revolutions per day: | 15.50495558 |
| mean anomaly at epoch: | 186.6941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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