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 62621U 26144.74141100 +.00000000 +00000-0 +13429-2 0 00006
2 62621 97.3966 227.6419 0002734 68.5728 291.5810 15.41186598 06
| Epoch (UTC): | 24 May 2026 17:47:37 |
| Eccentricity: | 0.0002734 |
| inclination: | 97.3966° |
| perigee height: | 441 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 227.6419° |
| argument of perigee: | 68.5728° |
| revolutions per day: | 15.41186598 |
| mean anomaly at epoch: | 291.5810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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