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 57673U 26145.43659955 +.00000000 +00000-0 +18150-4 0 00004
2 57673 53.1609 210.5941 0000994 86.6766 273.4349 15.30189595 05
| Epoch (UTC): | 25 May 2026 10:28:42 |
| Eccentricity: | 0.0000994 |
| inclination: | 53.1609° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.5941° |
| argument of perigee: | 86.6766° |
| revolutions per day: | 15.30189595 |
| mean anomaly at epoch: | 273.4349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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