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 56748U 26145.61878874 +.00000000 +00000-0 +29437-3 0 00008
2 56748 97.5128 343.3307 0007483 96.3204 263.8889 15.30872690 08
| Epoch (UTC): | 25 May 2026 14:51:03 |
| Eccentricity: | 0.0007483 |
| inclination: | 97.5128° |
| perigee height: | 468 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 343.3307° |
| argument of perigee: | 96.3204° |
| revolutions per day: | 15.30872690 |
| mean anomaly at epoch: | 263.8889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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