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 56063U 26145.55854962 +.00000000 +00000-0 +12010-3 0 00002
2 56063 87.9265 248.4745 0002168 98.2693 261.8687 13.21826717 03
| Epoch (UTC): | 25 May 2026 13:24:18 |
| Eccentricity: | 0.0002168 |
| inclination: | 87.9265° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4745° |
| argument of perigee: | 98.2693° |
| revolutions per day: | 13.21826717 |
| mean anomaly at epoch: | 261.8687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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