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 56203U 26145.59987218 +.00000000 +00000-0 +63372-3 0 00000
2 56203 97.2664 52.2890 0006399 23.0103 337.1437 15.55092772 05
| Epoch (UTC): | 25 May 2026 14:23:48 |
| Eccentricity: | 0.0006399 |
| inclination: | 97.2664° |
| perigee height: | 398 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 52.2890° |
| argument of perigee: | 23.0103° |
| revolutions per day: | 15.55092772 |
| mean anomaly at epoch: | 337.1437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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