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 21398U 26070.61706552 +.00000000 +00000-0 +53824-4 0 00009
2 21398 82.5227 134.6782 0021293 156.1678 204.0528 14.81843772 09
| Epoch (UTC): | 11 March 2026 14:48:34 |
| Eccentricity: | 0.0021293 |
| inclination: | 82.5227° |
| perigee height: | 609 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 134.6782° |
| argument of perigee: | 156.1678° |
| revolutions per day: | 14.81843772 |
| mean anomaly at epoch: | 204.0528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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