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 57532U 26145.12301740 +.00000000 +00000-0 +20560-4 0 00008
2 57532 43.0025 289.7080 0001523 269.0663 91.0014 15.27575205 09
| Epoch (UTC): | 25 May 2026 02:57:08 |
| Eccentricity: | 0.0001523 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 289.7080° |
| argument of perigee: | 269.0663° |
| revolutions per day: | 15.27575205 |
| mean anomaly at epoch: | 91.0014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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