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 45395U 26145.43509568 +.00000000 +00000-0 +48434-3 0 00003
2 45395 53.0409 116.0470 0006924 16.0377 344.0856 15.66547607 00
| Epoch (UTC): | 25 May 2026 10:26:32 |
| Eccentricity: | 0.0006924 |
| inclination: | 53.0409° |
| perigee height: | 364 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 116.0470° |
| argument of perigee: | 16.0377° |
| revolutions per day: | 15.66547607 |
| mean anomaly at epoch: | 344.0856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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