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 59204U 26145.41958833 +.00000000 +00000-0 +64893-4 0 00006
2 59204 53.1589 159.1927 0001158 93.8529 266.2604 15.30186905 02
| Epoch (UTC): | 25 May 2026 10:04:12 |
| Eccentricity: | 0.0001158 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 159.1927° |
| argument of perigee: | 93.8529° |
| revolutions per day: | 15.30186905 |
| mean anomaly at epoch: | 266.2604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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