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 52588U 26145.36180514 +.00000000 +00000-0 +41063-4 0 00005
2 52588 53.2129 134.9277 0000850 74.7748 285.3338 15.08842800 03
| Epoch (UTC): | 25 May 2026 08:40:59 |
| Eccentricity: | 0.0000850 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 134.9277° |
| argument of perigee: | 74.7748° |
| revolutions per day: | 15.08842800 |
| mean anomaly at epoch: | 285.3338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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