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 57438U 26145.47168544 +.00000000 +00000-0 +25850-4 0 00001
2 57438 42.9986 186.3128 0001465 268.6050 91.4634 15.27576962 06
| Epoch (UTC): | 25 May 2026 11:19:13 |
| Eccentricity: | 0.0001465 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.3128° |
| argument of perigee: | 268.6050° |
| revolutions per day: | 15.27576962 |
| mean anomaly at epoch: | 91.4634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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