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 56694U 26145.46342962 +.00000000 +00000-0 +18147-3 0 00001
2 56694 43.0032 200.7184 0001914 260.3852 99.6783 15.27578884 04
| Epoch (UTC): | 25 May 2026 11:07:20 |
| Eccentricity: | 0.0001914 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.7184° |
| argument of perigee: | 260.3852° |
| revolutions per day: | 15.27578884 |
| mean anomaly at epoch: | 99.6783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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