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 26088.17355154 +.00000000 +00000-0 +55591-4 0 00000
2 21398 82.5194 118.2766 0022224 101.4041 258.9671 14.81856788 02
| Epoch (UTC): | 29 March 2026 04:09:54 |
| Eccentricity: | 0.0022224 |
| inclination: | 82.5194° |
| perigee height: | 608 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 118.2766° |
| argument of perigee: | 101.4041° |
| revolutions per day: | 14.81856788 |
| mean anomaly at epoch: | 258.9671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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