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 62679U 26145.49965657 +.00000000 +00000-0 +12859-2 0 00009
2 62679 97.3922 226.8573 0003914 71.8671 288.2996 15.30399013 02
| Epoch (UTC): | 25 May 2026 11:59:30 |
| Eccentricity: | 0.0003914 |
| inclination: | 97.3922° |
| perigee height: | 472 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 226.8573° |
| argument of perigee: | 71.8671° |
| revolutions per day: | 15.30399013 |
| mean anomaly at epoch: | 288.2996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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