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 59947U 26145.42827104 +.00000000 +00000-0 +81192-5 0 00009
2 59947 53.1598 232.5879 0000700 115.5600 244.5491 15.69704465 04
| Epoch (UTC): | 25 May 2026 10:16:42 |
| Eccentricity: | 0.0000700 |
| inclination: | 53.1598° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 232.5879° |
| argument of perigee: | 115.5600° |
| revolutions per day: | 15.69704465 |
| mean anomaly at epoch: | 244.5491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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