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 51969U 26145.37317189 +.00000000 +00000-0 +85897-4 0 00001
2 51969 53.1610 27.6677 0001634 87.4369 272.6819 15.31702366 03
| Epoch (UTC): | 25 May 2026 08:57:22 |
| Eccentricity: | 0.0001634 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 27.6677° |
| argument of perigee: | 87.4369° |
| revolutions per day: | 15.31702366 |
| mean anomaly at epoch: | 272.6819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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