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 57452U 26145.59408447 +.00000000 +00000-0 +31232-3 0 00009
2 57452 35.0041 199.7624 0002044 212.4443 147.6147 15.23135323 04
| Epoch (UTC): | 25 May 2026 14:15:28 |
| Eccentricity: | 0.0002044 |
| inclination: | 35.0041° |
| perigee height: | 495 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 199.7624° |
| argument of perigee: | 212.4443° |
| revolutions per day: | 15.23135323 |
| mean anomaly at epoch: | 147.6147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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