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 52583U 26145.24404435 +.00000000 +00000-0 +52162-4 0 00000
2 52583 53.2154 135.4533 0001370 69.6322 290.4817 15.08845168 05
| Epoch (UTC): | 25 May 2026 05:51:25 |
| Eccentricity: | 0.0001370 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 135.4533° |
| argument of perigee: | 69.6322° |
| revolutions per day: | 15.08845168 |
| mean anomaly at epoch: | 290.4817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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