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 26064.67482878 +.00000000 +00000-0 +72541-4 0 00007
2 21398 82.5237 140.2279 0020816 175.2114 184.9303 14.81838060 02
| Epoch (UTC): | 05 March 2026 16:11:45 |
| Eccentricity: | 0.0020816 |
| inclination: | 82.5237° |
| perigee height: | 609 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 140.2279° |
| argument of perigee: | 175.2114° |
| revolutions per day: | 14.81838060 |
| mean anomaly at epoch: | 184.9303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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