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 59713U 26145.17242610 +.00000000 +00000-0 +21220-4 0 00000
2 59713 53.1593 309.3161 0000688 91.3658 268.7438 15.69710144 06
| Epoch (UTC): | 25 May 2026 04:08:17 |
| Eccentricity: | 0.0000688 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 309.3161° |
| argument of perigee: | 91.3658° |
| revolutions per day: | 15.69710144 |
| mean anomaly at epoch: | 268.7438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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