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 50177U 26145.07384705 +.00000000 +00000-0 +16033-4 0 00002
2 50177 53.2161 266.2171 0001386 102.9601 257.1546 15.08837364 07
| Epoch (UTC): | 25 May 2026 01:46:20 |
| Eccentricity: | 0.0001386 |
| inclination: | 53.2161° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 266.2171° |
| argument of perigee: | 102.9601° |
| revolutions per day: | 15.08837364 |
| mean anomaly at epoch: | 257.1546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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