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 59129U 26145.36705998 +.00000000 +00000-0 +36388-3 0 00005
2 59129 97.5445 294.3404 0004357 284.5043 75.5727 15.54561865 02
| Epoch (UTC): | 25 May 2026 08:48:33 |
| Eccentricity: | 0.0004357 |
| inclination: | 97.5445° |
| perigee height: | 400 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 294.3404° |
| argument of perigee: | 284.5043° |
| revolutions per day: | 15.54561865 |
| mean anomaly at epoch: | 75.5727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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