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 59201U 26145.42169900 +.00000000 +00000-0 +99318-5 0 00004
2 59201 53.1594 159.2079 0001202 83.1346 276.9792 15.30188929 07
| Epoch (UTC): | 25 May 2026 10:07:14 |
| Eccentricity: | 0.0001202 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 159.2079° |
| argument of perigee: | 83.1346° |
| revolutions per day: | 15.30188929 |
| mean anomaly at epoch: | 276.9792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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