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 52284U 26145.21644644 +.00000000 +00000-0 -85120-4 0 00004
2 52284 53.2138 115.5751 0001311 68.2170 291.8961 15.08847171 08
| Epoch (UTC): | 25 May 2026 05:11:40 |
| Eccentricity: | 0.0001311 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.5751° |
| argument of perigee: | 68.2170° |
| revolutions per day: | 15.08847171 |
| mean anomaly at epoch: | 291.8961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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