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 26040.94062369 +.00000000 +00000-0 +66229-4 0 00005
2 19039 74.0448 236.7766 0023421 343.7697 16.2705 14.39938085 00
| Epoch (UTC): | 09 February 2026 22:34:29 |
| Eccentricity: | 0.0023421 |
| inclination: | 74.0448° |
| perigee height: | 742 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 236.7766° |
| argument of perigee: | 343.7697° |
| revolutions per day: | 14.39938085 |
| mean anomaly at epoch: | 16.2705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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