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 26037.60580459 +.00000000 +00000-0 +97314-4 0 00008
2 19039 74.0451 242.9344 0023291 350.6687 9.4032 14.39937123 05
| Epoch (UTC): | 06 February 2026 14:32:21 |
| Eccentricity: | 0.0023291 |
| inclination: | 74.0451° |
| perigee height: | 742 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 242.9344° |
| argument of perigee: | 350.6687° |
| revolutions per day: | 14.39937123 |
| mean anomaly at epoch: | 9.4032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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