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 57613U 26145.02586494 +.00000000 +00000-0 +47266-4 0 00000
2 57613 43.0034 10.2436 0001775 266.9880 93.0768 15.27575091 08
| Epoch (UTC): | 25 May 2026 00:37:14 |
| Eccentricity: | 0.0001775 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.2436° |
| argument of perigee: | 266.9880° |
| revolutions per day: | 15.27575091 |
| mean anomaly at epoch: | 93.0768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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