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 32384U 26144.85454153 +.00000000 +00000-0 +00000-0 0 00005
2 32384 55.0511 275.0902 0035292 164.1144 9.0351 2.00558668 04
| Epoch (UTC): | 24 May 2026 20:30:32 |
| Eccentricity: | 0.0035292 |
| inclination: | 55.0511° |
| perigee height: | 20089 km |
| apogee height: | 20276 km |
| right ascension of ascending node: | 275.0902° |
| argument of perigee: | 164.1144° |
| revolutions per day: | 2.00558668 |
| mean anomaly at epoch: | 9.0351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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