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 53919U 26145.52020243 +.00000000 +00000-0 +57913-4 0 00005
2 53919 53.2160 327.8275 0001129 92.8694 267.2430 15.14833083 01
| Epoch (UTC): | 25 May 2026 12:29:05 |
| Eccentricity: | 0.0001129 |
| inclination: | 53.2160° |
| perigee height: | 521 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 327.8275° |
| argument of perigee: | 92.8694° |
| revolutions per day: | 15.14833083 |
| mean anomaly at epoch: | 267.2430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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