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 51883U 26145.35815142 +.00000000 +00000-0 +22653-3 0 00006
2 51883 53.2132 15.1239 0001182 87.4697 272.6430 15.08829051 00
| Epoch (UTC): | 25 May 2026 08:35:44 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 15.1239° |
| argument of perigee: | 87.4697° |
| revolutions per day: | 15.08829051 |
| mean anomaly at epoch: | 272.6430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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