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 50173U 26145.00899676 +.00000000 +00000-0 +96436-3 0 00003
2 50173 53.2147 254.8785 0000698 125.5317 234.5743 15.13058666 05
| Epoch (UTC): | 25 May 2026 00:12:57 |
| Eccentricity: | 0.0000698 |
| inclination: | 53.2147° |
| perigee height: | 526 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 254.8785° |
| argument of perigee: | 125.5317° |
| revolutions per day: | 15.13058666 |
| mean anomaly at epoch: | 234.5743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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