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 19039U 26044.90071749 +.00000000 +00000-0 +62302-4 0 00005
2 19039 74.0449 229.4637 0023624 335.4911 24.5119 14.39939561 00
| Epoch (UTC): | 13 February 2026 21:37:01 |
| Eccentricity: | 0.0023624 |
| inclination: | 74.0449° |
| perigee height: | 742 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 229.4637° |
| argument of perigee: | 335.4911° |
| revolutions per day: | 14.39939561 |
| mean anomaly at epoch: | 24.5119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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