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 62697U 26145.59442653 +.00000000 +00000-0 +13140-3 0 00001
2 62697 97.7046 224.3178 0003863 87.4868 272.6795 14.94302015 00
| Epoch (UTC): | 25 May 2026 14:15:58 |
| Eccentricity: | 0.0003863 |
| inclination: | 97.7046° |
| perigee height: | 582 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 224.3178° |
| argument of perigee: | 87.4868° |
| revolutions per day: | 14.94302015 |
| mean anomaly at epoch: | 272.6795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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