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 51858U 26145.41149221 +.00000000 +00000-0 +15184-3 0 00004
2 51858 53.2119 34.7040 0001079 90.4093 269.7022 15.08827723 01
| Epoch (UTC): | 25 May 2026 09:52:32 |
| Eccentricity: | 0.0001079 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.7040° |
| argument of perigee: | 90.4093° |
| revolutions per day: | 15.08827723 |
| mean anomaly at epoch: | 269.7022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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