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 52688U 26145.36133617 +.00000000 +00000-0 +37317-4 0 00005
2 52688 53.2127 159.8127 0001121 108.7125 251.3988 15.08839892 02
| Epoch (UTC): | 25 May 2026 08:40:19 |
| Eccentricity: | 0.0001121 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 159.8127° |
| argument of perigee: | 108.7125° |
| revolutions per day: | 15.08839892 |
| mean anomaly at epoch: | 251.3988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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