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 21232U 26087.94075020 +.00000000 +00000-0 -41208-3 0 00002
2 21232 82.5404 241.0719 0012824 4.1919 110.1727 13.16699055 04
| Epoch (UTC): | 28 March 2026 22:34:40 |
| Eccentricity: | 0.0012824 |
| inclination: | 82.5404° |
| perigee height: | 1188 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 241.0719° |
| argument of perigee: | 4.1919° |
| revolutions per day: | 13.16699055 |
| mean anomaly at epoch: | 110.1727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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