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 45369U 26145.28022985 +.00000000 +00000-0 +10136-2 0 00007
2 45369 53.0437 142.0133 0006678 1.2685 358.8343 15.61509576 03
| Epoch (UTC): | 25 May 2026 06:43:31 |
| Eccentricity: | 0.0006678 |
| inclination: | 53.0437° |
| perigee height: | 379 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 142.0133° |
| argument of perigee: | 1.2685° |
| revolutions per day: | 15.61509576 |
| mean anomaly at epoch: | 358.8343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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