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 57676U 26145.35336139 +.00000000 +00000-0 +32465-4 0 00009
2 57676 53.1598 210.8878 0000960 92.3809 267.7302 15.30193375 08
| Epoch (UTC): | 25 May 2026 08:28:50 |
| Eccentricity: | 0.0000960 |
| inclination: | 53.1598° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.8878° |
| argument of perigee: | 92.3809° |
| revolutions per day: | 15.30193375 |
| mean anomaly at epoch: | 267.7302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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