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 26070.72047230 +.00000000 +00000-0 +32719-3 0 00001
2 19210 82.5103 156.2051 0012555 116.2836 243.9695 15.28565914 03
| Epoch (UTC): | 11 March 2026 17:17:28 |
| Eccentricity: | 0.0012555 |
| inclination: | 82.5103° |
| perigee height: | 471 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 156.2051° |
| argument of perigee: | 116.2836° |
| revolutions per day: | 15.28565914 |
| mean anomaly at epoch: | 243.9695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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