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 57728U 26145.60556074 +.00000000 +00000-0 +28074-3 0 00007
2 57728 34.9947 292.6714 0009727 242.5238 117.4486 15.16030925 02
| Epoch (UTC): | 25 May 2026 14:32:00 |
| Eccentricity: | 0.0009727 |
| inclination: | 34.9947° |
| perigee height: | 511 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 292.6714° |
| argument of perigee: | 242.5238° |
| revolutions per day: | 15.16030925 |
| mean anomaly at epoch: | 117.4486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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