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 51768U 26144.86316397 +.00000000 +00000-0 +43717-4 0 00006
2 51768 53.2166 357.1651 0001468 94.4730 265.6430 15.08842706 03
| Epoch (UTC): | 24 May 2026 20:42:57 |
| Eccentricity: | 0.0001468 |
| inclination: | 53.2166° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 357.1651° |
| argument of perigee: | 94.4730° |
| revolutions per day: | 15.08842706 |
| mean anomaly at epoch: | 265.6430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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