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 62710U 26145.59382013 +.00000000 +00000-0 +98087-4 0 00004
2 62710 97.7061 224.2293 0002691 220.5616 139.5403 14.92819929 01
| Epoch (UTC): | 25 May 2026 14:15:06 |
| Eccentricity: | 0.0002691 |
| inclination: | 97.7061° |
| perigee height: | 587 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 224.2293° |
| argument of perigee: | 220.5616° |
| revolutions per day: | 14.92819929 |
| mean anomaly at epoch: | 139.5403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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