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 62699U 26145.51148377 +.00000000 +00000-0 +67074-3 0 00006
2 62699 97.6850 227.0855 0002238 190.9292 169.1884 15.02050290 06
| Epoch (UTC): | 25 May 2026 12:16:32 |
| Eccentricity: | 0.0002238 |
| inclination: | 97.6850° |
| perigee height: | 559 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 227.0855° |
| argument of perigee: | 190.9292° |
| revolutions per day: | 15.02050290 |
| mean anomaly at epoch: | 169.1884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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