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 26085.97542414 +.00000000 +00000-0 +00000-0 0 00001
2 19687 13.1788 337.4898 0007027 320.3596 235.2088 0.99676546 07
| Epoch (UTC): | 26 March 2026 23:24:36 |
| Eccentricity: | 0.0007027 |
| inclination: | 13.1788° |
| perigee height: | 35925 km |
| apogee height: | 35984 km |
| right ascension of ascending node: | 337.4898° |
| argument of perigee: | 320.3596° |
| revolutions per day: | 0.99676546 |
| mean anomaly at epoch: | 235.2088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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