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 59202U 26145.30454074 +.00000000 +00000-0 +22745-4 0 00000
2 59202 53.1603 158.4806 0001178 87.6387 272.4750 15.34390120 01
| Epoch (UTC): | 25 May 2026 07:18:32 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 158.4806° |
| argument of perigee: | 87.6387° |
| revolutions per day: | 15.34390120 |
| mean anomaly at epoch: | 272.4750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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