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 56361U 26145.43580561 +.00000000 +00000-0 -11973-4 0 00000
2 56361 97.4460 145.4105 0001589 81.9510 278.1898 15.05650736 01
| Epoch (UTC): | 25 May 2026 10:27:33 |
| Eccentricity: | 0.0001589 |
| inclination: | 97.4460° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.4105° |
| argument of perigee: | 81.9510° |
| revolutions per day: | 15.05650736 |
| mean anomaly at epoch: | 278.1898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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