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 62159U 26145.54287953 +.00000000 +00000-0 +72432-3 0 00008
2 62159 43.0017 87.5458 0001078 251.1436 108.9299 15.27576942 01
| Epoch (UTC): | 25 May 2026 13:01:44 |
| Eccentricity: | 0.0001078 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.5458° |
| argument of perigee: | 251.1436° |
| revolutions per day: | 15.27576942 |
| mean anomaly at epoch: | 108.9299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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