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 57134U 26145.56088406 +.00000000 +00000-0 +13583-4 0 00002
2 57134 43.0028 188.8951 0001069 296.7954 63.2788 15.27572435 02
| Epoch (UTC): | 25 May 2026 13:27:40 |
| Eccentricity: | 0.0001069 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 188.8951° |
| argument of perigee: | 296.7954° |
| revolutions per day: | 15.27572435 |
| mean anomaly at epoch: | 63.2788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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