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 57412U 26145.54220074 +.00000000 +00000-0 +25315-4 0 00004
2 57412 43.0046 174.5453 0002013 267.4032 92.6590 15.27574584 06
| Epoch (UTC): | 25 May 2026 13:00:46 |
| Eccentricity: | 0.0002013 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.5453° |
| argument of perigee: | 267.4032° |
| revolutions per day: | 15.27574584 |
| mean anomaly at epoch: | 92.6590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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