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 26041.98275405 +.00000000 +00000-0 +65614-4 0 00004
2 19039 74.0449 234.8524 0023467 341.6235 18.4069 14.39938484 07
| Epoch (UTC): | 10 February 2026 23:35:09 |
| Eccentricity: | 0.0023467 |
| inclination: | 74.0449° |
| perigee height: | 742 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 234.8524° |
| argument of perigee: | 341.6235° |
| revolutions per day: | 14.39938484 |
| mean anomaly at epoch: | 18.4069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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