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 57381U 26145.49291003 +.00000000 +00000-0 +77513-4 0 00000
2 57381 43.0027 149.9462 0001010 285.5489 74.5251 15.27587010 00
| Epoch (UTC): | 25 May 2026 11:49:47 |
| Eccentricity: | 0.0001010 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.9462° |
| argument of perigee: | 285.5489° |
| revolutions per day: | 15.27587010 |
| mean anomaly at epoch: | 74.5251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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