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 62910U 26145.62698804 +.00000000 +00000-0 +13019-2 0 00008
2 62910 43.0020 243.7964 0002152 277.3282 82.7341 15.70802096 08
| Epoch (UTC): | 25 May 2026 15:02:51 |
| Eccentricity: | 0.0002152 |
| inclination: | 43.0020° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 243.7964° |
| argument of perigee: | 277.3282° |
| revolutions per day: | 15.70802096 |
| mean anomaly at epoch: | 82.7341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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