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 52307U 26145.29372840 +.00000000 +00000-0 -77980-4 0 00009
2 52307 53.2143 115.2301 0001165 94.6228 265.4897 15.08846477 05
| Epoch (UTC): | 25 May 2026 07:02:58 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.2301° |
| argument of perigee: | 94.6228° |
| revolutions per day: | 15.08846477 |
| mean anomaly at epoch: | 265.4897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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