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 56534U 26145.38839199 +.00000000 +00000-0 +21066-5 0 00004
2 56534 42.9993 125.1455 0000961 315.8258 44.2517 15.27575970 03
| Epoch (UTC): | 25 May 2026 09:19:17 |
| Eccentricity: | 0.0000961 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.1455° |
| argument of perigee: | 315.8258° |
| revolutions per day: | 15.27575970 |
| mean anomaly at epoch: | 44.2517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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