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 19687U 26102.07266877 +.00000000 +00000-0 +00000-0 0 00008
2 19687 13.1639 337.3778 0006396 322.9190 249.0707 0.99674729 06
| Epoch (UTC): | 12 April 2026 01:44:38 |
| Eccentricity: | 0.0006396 |
| inclination: | 13.1639° |
| perigee height: | 35928 km |
| apogee height: | 35982 km |
| right ascension of ascending node: | 337.3778° |
| argument of perigee: | 322.9190° |
| revolutions per day: | 0.99674729 |
| mean anomaly at epoch: | 249.0707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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