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 45383U 26145.58335647 +.00000000 +00000-0 +11861-1 0 00003
2 45383 53.0430 123.0779 0001647 86.3635 2.3824 15.62322339 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001647 |
| inclination: | 53.0430° |
| perigee height: | 380 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 123.0779° |
| argument of perigee: | 86.3635° |
| revolutions per day: | 15.62322339 |
| mean anomaly at epoch: | 2.3824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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