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 59424U 26145.23059905 +.00000000 +00000-0 +32943-4 0 00003
2 59424 53.1580 76.6406 0001294 127.9761 232.1374 15.69723280 01
| Epoch (UTC): | 25 May 2026 05:32:03 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.1580° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 76.6406° |
| argument of perigee: | 127.9761° |
| revolutions per day: | 15.69723280 |
| mean anomaly at epoch: | 232.1374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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