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 56492U 26145.40019632 +.00000000 +00000-0 +97634-4 0 00005
2 56492 69.9987 271.0109 0002534 271.7789 88.3080 14.98326885 02
| Epoch (UTC): | 25 May 2026 09:36:16 |
| Eccentricity: | 0.0002534 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 271.0109° |
| argument of perigee: | 271.7789° |
| revolutions per day: | 14.98326885 |
| mean anomaly at epoch: | 88.3080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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