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 57468U 26145.38267902 +.00000000 +00000-0 +12546-3 0 00009
2 57468 43.0020 263.2104 0001183 261.9448 98.1269 15.27583497 02
| Epoch (UTC): | 25 May 2026 09:11:03 |
| Eccentricity: | 0.0001183 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.2104° |
| argument of perigee: | 261.9448° |
| revolutions per day: | 15.27583497 |
| mean anomaly at epoch: | 98.1269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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