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 57677U 26145.44071906 +.00000000 +00000-0 +23434-4 0 00004
2 57677 53.1595 209.9770 0001165 85.8959 274.2175 15.30189215 06
| Epoch (UTC): | 25 May 2026 10:34:38 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.9770° |
| argument of perigee: | 85.8959° |
| revolutions per day: | 15.30189215 |
| mean anomaly at epoch: | 274.2175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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