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 26040.52377147 +.00000000 +00000-0 +70094-4 0 00007
2 19039 74.0448 237.5464 0023404 344.6489 15.3953 14.39938003 09
| Epoch (UTC): | 09 February 2026 12:34:13 |
| Eccentricity: | 0.0023404 |
| inclination: | 74.0448° |
| perigee height: | 742 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 237.5464° |
| argument of perigee: | 344.6489° |
| revolutions per day: | 14.39938003 |
| mean anomaly at epoch: | 15.3953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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