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 57504U 26145.47258854 +.00000000 +00000-0 +11251-3 0 00008
2 57504 42.9989 302.8132 0001128 273.0671 87.0051 15.27581854 08
| Epoch (UTC): | 25 May 2026 11:20:31 |
| Eccentricity: | 0.0001128 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.8132° |
| argument of perigee: | 273.0671° |
| revolutions per day: | 15.27581854 |
| mean anomaly at epoch: | 87.0051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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