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 57748U 26145.34399925 +.00000000 +00000-0 +63870-4 0 00004
2 57748 43.0038 99.2164 0001191 270.5180 89.5536 15.27583093 06
| Epoch (UTC): | 25 May 2026 08:15:21 |
| Eccentricity: | 0.0001191 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.2164° |
| argument of perigee: | 270.5180° |
| revolutions per day: | 15.27583093 |
| mean anomaly at epoch: | 89.5536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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