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 62110U 26145.40671618 +.00000000 +00000-0 +43442-3 0 00004
2 62110 43.0018 132.3230 0001449 270.4717 89.5969 15.27594393 02
| Epoch (UTC): | 25 May 2026 09:45:40 |
| Eccentricity: | 0.0001449 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.3230° |
| argument of perigee: | 270.4717° |
| revolutions per day: | 15.27594393 |
| mean anomaly at epoch: | 89.5969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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