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 57731U 26145.60104332 +.00000000 +00000-0 +29668-3 0 00007
2 57731 34.9936 292.6102 0009019 116.5381 243.6257 15.15989899 08
| Epoch (UTC): | 25 May 2026 14:25:30 |
| Eccentricity: | 0.0009019 |
| inclination: | 34.9936° |
| perigee height: | 512 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 292.6102° |
| argument of perigee: | 116.5381° |
| revolutions per day: | 15.15989899 |
| mean anomaly at epoch: | 243.6257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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