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 52364U 26145.54303853 +.00000000 +00000-0 -64323-4 0 00005
2 52364 53.2097 204.0244 0001248 103.0775 257.0356 15.08835550 00
| Epoch (UTC): | 25 May 2026 13:01:58 |
| Eccentricity: | 0.0001248 |
| inclination: | 53.2097° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 204.0244° |
| argument of perigee: | 103.0775° |
| revolutions per day: | 15.08835550 |
| mean anomaly at epoch: | 257.0356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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