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 21397U 26065.62019389 +.00000000 +00000-0 +31051-3 0 00005
2 21397 82.5192 339.8166 0014115 349.6073 10.4860 15.04777037 01
| Epoch (UTC): | 06 March 2026 14:53:04 |
| Eccentricity: | 0.0014115 |
| inclination: | 82.5192° |
| perigee height: | 542 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 339.8166° |
| argument of perigee: | 349.6073° |
| revolutions per day: | 15.04777037 |
| mean anomaly at epoch: | 10.4860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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