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 52686U 26145.34025998 +.00000000 +00000-0 +12860-3 0 00008
2 52686 53.2113 160.3014 0001536 80.6159 279.5006 15.08831097 04
| Epoch (UTC): | 25 May 2026 08:09:58 |
| Eccentricity: | 0.0001536 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 160.3014° |
| argument of perigee: | 80.6159° |
| revolutions per day: | 15.08831097 |
| mean anomaly at epoch: | 279.5006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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