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 19419U 26053.68627453 +.00000000 +00000-0 +19270-3 0 00006
2 19419 90.0393 20.4820 0097607 41.9076 136.7508 13.42638192 01
| Epoch (UTC): | 22 February 2026 16:28:14 |
| Eccentricity: | 0.0097607 |
| inclination: | 90.0393° |
| perigee height: | 1026 km |
| apogee height: | 1172 km |
| right ascension of ascending node: | 20.4820° |
| argument of perigee: | 41.9076° |
| revolutions per day: | 13.42638192 |
| mean anomaly at epoch: | 136.7508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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