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 56463U 26145.46324553 +.00000000 +00000-0 +49465-4 0 00009
2 56463 69.9987 310.9662 0002655 263.0084 97.0773 14.98329378 09
| Epoch (UTC): | 25 May 2026 11:07:04 |
| Eccentricity: | 0.0002655 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.9662° |
| argument of perigee: | 263.0084° |
| revolutions per day: | 14.98329378 |
| mean anomaly at epoch: | 97.0773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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