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 19508U 26149.92577850 +.00000000 +00000-0 +00000-0 0 00001
2 19508 14.8954 353.8428 0005181 337.5179 214.6854 0.99226404 05
| Epoch (UTC): | 29 May 2026 22:13:07 |
| Eccentricity: | 0.0005181 |
| inclination: | 14.8954° |
| perigee height: | 36060 km |
| apogee height: | 36104 km |
| right ascension of ascending node: | 353.8428° |
| argument of perigee: | 337.5179° |
| revolutions per day: | 0.99226404 |
| mean anomaly at epoch: | 214.6854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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