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 62815U 26145.18713584 +.00000000 +00000-0 +51400-3 0 00003
2 62815 53.1601 314.0492 0000406 110.0882 250.0162 15.30211344 03
| Epoch (UTC): | 25 May 2026 04:29:28 |
| Eccentricity: | 0.0000406 |
| inclination: | 53.1601° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 314.0492° |
| argument of perigee: | 110.0882° |
| revolutions per day: | 15.30211344 |
| mean anomaly at epoch: | 250.0162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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