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 19071U 26053.63339181 +.00000000 +00000-0 +14867-3 0 00000
2 19071 90.3270 18.7620 0186998 327.8519 210.0356 13.27966011 04
| Epoch (UTC): | 22 February 2026 15:12:05 |
| Eccentricity: | 0.0186998 |
| inclination: | 90.3270° |
| perigee height: | 1014 km |
| apogee height: | 1295 km |
| right ascension of ascending node: | 18.7620° |
| argument of perigee: | 327.8519° |
| revolutions per day: | 13.27966011 |
| mean anomaly at epoch: | 210.0356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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