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 19420U 26053.63678581 +.00000000 +00000-0 +15253-3 0 00008
2 19420 90.0410 20.8435 0095663 36.3913 136.4649 13.42595150 06
| Epoch (UTC): | 22 February 2026 15:16:58 |
| Eccentricity: | 0.0095663 |
| inclination: | 90.0410° |
| perigee height: | 1028 km |
| apogee height: | 1171 km |
| right ascension of ascending node: | 20.8435° |
| argument of perigee: | 36.3913° |
| revolutions per day: | 13.42595150 |
| mean anomaly at epoch: | 136.4649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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