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 56157U 26145.64060675 +.00000000 +00000-0 +22423-4 0 00006
2 56157 63.3997 156.2631 0065234 354.9736 5.0628 13.45389185 02
| Epoch (UTC): | 25 May 2026 15:22:28 |
| Eccentricity: | 0.0065234 |
| inclination: | 63.3997° |
| perigee height: | 1041 km |
| apogee height: | 1138 km |
| right ascension of ascending node: | 156.2631° |
| argument of perigee: | 354.9736° |
| revolutions per day: | 13.45389185 |
| mean anomaly at epoch: | 5.0628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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