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 62657U 26144.47209174 +.00000000 +00000-0 +25228-3 0 00002
2 62657 97.3944 226.3383 0002193 51.3441 308.7995 15.28548902 09
| Epoch (UTC): | 24 May 2026 11:19:48 |
| Eccentricity: | 0.0002193 |
| inclination: | 97.3944° |
| perigee height: | 479 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 226.3383° |
| argument of perigee: | 51.3441° |
| revolutions per day: | 15.28548902 |
| mean anomaly at epoch: | 308.7995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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