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 65381U 26145.57920833 +.00000000 +00000-0 +19558-3 0 00002
2 65381 97.4524 17.0006 0002331 104.6156 255.5330 15.05654231 07
| Epoch (UTC): | 25 May 2026 13:54:03 |
| Eccentricity: | 0.0002331 |
| inclination: | 97.4524° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.0006° |
| argument of perigee: | 104.6156° |
| revolutions per day: | 15.05654231 |
| mean anomaly at epoch: | 255.5330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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