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 57611U 26145.61305104 +.00000000 +00000-0 -24458-4 0 00009
2 57611 43.0084 6.9143 0001396 262.5478 97.5215 15.27585466 05
| Epoch (UTC): | 25 May 2026 14:42:47 |
| Eccentricity: | 0.0001396 |
| inclination: | 43.0084° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 6.9143° |
| argument of perigee: | 262.5478° |
| revolutions per day: | 15.27585466 |
| mean anomaly at epoch: | 97.5215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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