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 57873U 26145.23900252 +.00000000 +00000-0 -31243-5 0 00003
2 57873 43.0035 212.9834 0001309 278.0521 82.0182 15.27575541 07
| Epoch (UTC): | 25 May 2026 05:44:09 |
| Eccentricity: | 0.0001309 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.9834° |
| argument of perigee: | 278.0521° |
| revolutions per day: | 15.27575541 |
| mean anomaly at epoch: | 82.0182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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