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 26074.26342677 +.00000000 +00000-0 +44841-4 0 00007
2 21398 82.5219 131.2724 0021593 144.5288 215.7367 14.81846682 03
| Epoch (UTC): | 15 March 2026 06:19:20 |
| Eccentricity: | 0.0021593 |
| inclination: | 82.5219° |
| perigee height: | 608 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 131.2724° |
| argument of perigee: | 144.5288° |
| revolutions per day: | 14.81846682 |
| mean anomaly at epoch: | 215.7367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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