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 50159U 26144.60653378 +.00000000 +00000-0 -73270-5 0 00003
2 50159 53.2158 278.3277 0001510 96.5589 263.5575 15.08830735 04
| Epoch (UTC): | 24 May 2026 14:33:24 |
| Eccentricity: | 0.0001510 |
| inclination: | 53.2158° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 278.3277° |
| argument of perigee: | 96.5589° |
| revolutions per day: | 15.08830735 |
| mean anomaly at epoch: | 263.5575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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