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 56323U 26145.43303660 +.00000000 +00000-0 +18295-3 0 00003
2 56323 97.4463 145.4099 0001021 63.8572 296.2760 15.05658009 02
| Epoch (UTC): | 25 May 2026 10:23:34 |
| Eccentricity: | 0.0001021 |
| inclination: | 97.4463° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 145.4099° |
| argument of perigee: | 63.8572° |
| revolutions per day: | 15.05658009 |
| mean anomaly at epoch: | 296.2760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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