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 26041.91327869 +.00000000 +00000-0 +66244-4 0 00009
2 19039 74.0449 234.9807 0023461 341.7690 18.2621 14.39938467 05
| Epoch (UTC): | 10 February 2026 21:55:07 |
| Eccentricity: | 0.0023461 |
| inclination: | 74.0449° |
| perigee height: | 742 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 234.9807° |
| argument of perigee: | 341.7690° |
| revolutions per day: | 14.39938467 |
| mean anomaly at epoch: | 18.2621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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