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 59100U 26145.56150544 +.00000000 +00000-0 +25824-3 0 00000
2 59100 97.8371 288.6942 0003536 140.9017 219.2469 15.12610371 00
| Epoch (UTC): | 25 May 2026 13:28:34 |
| Eccentricity: | 0.0003536 |
| inclination: | 97.8371° |
| perigee height: | 526 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 288.6942° |
| argument of perigee: | 140.9017° |
| revolutions per day: | 15.12610371 |
| mean anomaly at epoch: | 219.2469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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