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 50176U 26145.32777181 +.00000000 +00000-0 +18776-4 0 00009
2 50176 53.2143 265.0774 0000979 84.0563 276.0541 15.08833398 04
| Epoch (UTC): | 25 May 2026 07:51:59 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 265.0774° |
| argument of perigee: | 84.0563° |
| revolutions per day: | 15.08833398 |
| mean anomaly at epoch: | 276.0541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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