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 57023U 26145.58925690 +.00000000 +00000-0 +44755-3 0 00000
2 57023 97.4923 256.9015 0006966 141.2204 218.9539 15.32932432 03
| Epoch (UTC): | 25 May 2026 14:08:31 |
| Eccentricity: | 0.0006966 |
| inclination: | 97.4923° |
| perigee height: | 462 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 256.9015° |
| argument of perigee: | 141.2204° |
| revolutions per day: | 15.32932432 |
| mean anomaly at epoch: | 218.9539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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