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 32393U 26145.16821913 +.00000000 +00000-0 +00000-0 0 00002
2 32393 64.3161 192.6922 0001051 357.7939 81.0284 2.13101329 09
| Epoch (UTC): | 25 May 2026 04:02:14 |
| Eccentricity: | 0.0001051 |
| inclination: | 64.3161° |
| perigee height: | 19127 km |
| apogee height: | 19133 km |
| right ascension of ascending node: | 192.6922° |
| argument of perigee: | 357.7939° |
| revolutions per day: | 2.13101329 |
| mean anomaly at epoch: | 81.0284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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