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 57998U 26145.62258388 +.00000000 +00000-0 +27181-4 0 00004
2 57998 43.0068 352.4615 0001636 261.5856 98.4811 15.27578554 06
| Epoch (UTC): | 25 May 2026 14:56:31 |
| Eccentricity: | 0.0001636 |
| inclination: | 43.0068° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.4615° |
| argument of perigee: | 261.5856° |
| revolutions per day: | 15.27578554 |
| mean anomaly at epoch: | 98.4811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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