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 26162.58940707 +.00000000 +00000-0 +58126-4 0 00008
2 19039 74.0479 12.1701 0022316 91.6470 268.7241 14.40003641 01
| Epoch (UTC): | 11 June 2026 14:08:44 |
| Eccentricity: | 0.0022316 |
| inclination: | 74.0479° |
| perigee height: | 743 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 12.1701° |
| argument of perigee: | 91.6470° |
| revolutions per day: | 14.40003641 |
| mean anomaly at epoch: | 268.7241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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