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 59948U 26145.41363713 +.00000000 +00000-0 +58546-4 0 00006
2 59948 53.1599 233.2418 0001097 67.6146 292.4988 15.69735230 02
| Epoch (UTC): | 25 May 2026 09:55:38 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.1599° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 233.2418° |
| argument of perigee: | 67.6146° |
| revolutions per day: | 15.69735230 |
| mean anomaly at epoch: | 292.4988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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