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 59557U 26145.42776758 +.00000000 +00000-0 +37690-3 0 00006
2 59557 35.0010 52.7315 0006402 315.4474 44.5725 15.23048482 09
| Epoch (UTC): | 25 May 2026 10:15:59 |
| Eccentricity: | 0.0006402 |
| inclination: | 35.0010° |
| perigee height: | 492 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 52.7315° |
| argument of perigee: | 315.4474° |
| revolutions per day: | 15.23048482 |
| mean anomaly at epoch: | 44.5725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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