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 19210U 26065.35232760 +.00000000 +00000-0 +36586-3 0 00004
2 19210 82.5105 161.6021 0012387 133.2104 227.0173 15.28452731 08
| Epoch (UTC): | 06 March 2026 08:27:21 |
| Eccentricity: | 0.0012387 |
| inclination: | 82.5105° |
| perigee height: | 472 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 161.6021° |
| argument of perigee: | 133.2104° |
| revolutions per day: | 15.28452731 |
| mean anomaly at epoch: | 227.0173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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