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 62287U 26145.46687786 +.00000000 +00000-0 +49666-3 0 00002
2 62287 43.0006 142.7887 0001545 269.4827 90.5848 15.27594741 09
| Epoch (UTC): | 25 May 2026 11:12:18 |
| Eccentricity: | 0.0001545 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 142.7887° |
| argument of perigee: | 269.4827° |
| revolutions per day: | 15.27594741 |
| mean anomaly at epoch: | 90.5848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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