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 57230U 26145.52975899 +.00000000 +00000-0 -62952-5 0 00002
2 57230 43.0052 317.0711 0001562 273.9993 86.0680 15.27574245 09
| Epoch (UTC): | 25 May 2026 12:42:51 |
| Eccentricity: | 0.0001562 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.0711° |
| argument of perigee: | 273.9993° |
| revolutions per day: | 15.27574245 |
| mean anomaly at epoch: | 86.0680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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