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 57530U 26145.11915833 +.00000000 +00000-0 -57930-4 0 00001
2 57530 43.0033 289.6885 0002122 265.9394 94.1215 15.27587218 04
| Epoch (UTC): | 25 May 2026 02:51:35 |
| Eccentricity: | 0.0002122 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 289.6885° |
| argument of perigee: | 265.9394° |
| revolutions per day: | 15.27587218 |
| mean anomaly at epoch: | 94.1215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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