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 52760U 26145.41455391 +.00000000 +00000-0 +20350-3 0 00006
2 52760 97.6572 284.7948 0008103 194.6187 165.4818 15.26999915 07
| Epoch (UTC): | 25 May 2026 09:56:57 |
| Eccentricity: | 0.0008103 |
| inclination: | 97.6572° |
| perigee height: | 479 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 284.7948° |
| argument of perigee: | 194.6187° |
| revolutions per day: | 15.26999915 |
| mean anomaly at epoch: | 165.4818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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