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 59242U 26145.19518551 +.00000000 +00000-0 -12666-3 0 00003
2 59242 43.0037 71.7246 0001151 269.7997 90.2723 15.27606445 08
| Epoch (UTC): | 25 May 2026 04:41:04 |
| Eccentricity: | 0.0001151 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.7246° |
| argument of perigee: | 269.7997° |
| revolutions per day: | 15.27606445 |
| mean anomaly at epoch: | 90.2723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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