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 56328U 26145.43161647 +.00000000 +00000-0 +21084-4 0 00006
2 56328 97.4465 146.4782 0001413 81.4060 278.7328 15.05655898 00
| Epoch (UTC): | 25 May 2026 10:21:31 |
| Eccentricity: | 0.0001413 |
| inclination: | 97.4465° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 146.4782° |
| argument of perigee: | 81.4060° |
| revolutions per day: | 15.05655898 |
| mean anomaly at epoch: | 278.7328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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