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 57744U 26145.17023269 +.00000000 +00000-0 -34974-4 0 00000
2 57744 43.0068 86.0201 0001841 252.7040 107.3610 15.27573819 07
| Epoch (UTC): | 25 May 2026 04:05:08 |
| Eccentricity: | 0.0001841 |
| inclination: | 43.0068° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 86.0201° |
| argument of perigee: | 252.7040° |
| revolutions per day: | 15.27573819 |
| mean anomaly at epoch: | 107.3610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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