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 56376U 26145.38956529 +.00000000 +00000-0 +70170-4 0 00004
2 56376 43.0041 124.4202 0001107 288.6757 71.3974 15.27577751 06
| Epoch (UTC): | 25 May 2026 09:20:58 |
| Eccentricity: | 0.0001107 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.4202° |
| argument of perigee: | 288.6757° |
| revolutions per day: | 15.27577751 |
| mean anomaly at epoch: | 71.3974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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