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 19919U 26150.42460309 +.00000000 +00000-0 +00000-0 0 00004
2 19919 14.8896 352.4786 0003605 162.3154 209.9082 0.99174490 01
| Epoch (UTC): | 30 May 2026 10:11:25 |
| Eccentricity: | 0.0003605 |
| inclination: | 14.8896° |
| perigee height: | 36082 km |
| apogee height: | 36112 km |
| right ascension of ascending node: | 352.4786° |
| argument of perigee: | 162.3154° |
| revolutions per day: | 0.99174490 |
| mean anomaly at epoch: | 209.9082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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