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 59715U 26145.47607189 +.00000000 +00000-0 +16052-3 0 00007
2 59715 53.1586 307.6450 0000790 123.4837 236.6257 15.69653456 07
| Epoch (UTC): | 25 May 2026 11:25:32 |
| Eccentricity: | 0.0000790 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 307.6450° |
| argument of perigee: | 123.4837° |
| revolutions per day: | 15.69653456 |
| mean anomaly at epoch: | 236.6257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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