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 59351U 26145.46656222 +.00000000 +00000-0 -24535-4 0 00001
2 59351 42.9985 186.3630 0001492 272.3930 87.6751 15.27582854 02
| Epoch (UTC): | 25 May 2026 11:11:50 |
| Eccentricity: | 0.0001492 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.3630° |
| argument of perigee: | 272.3930° |
| revolutions per day: | 15.27582854 |
| mean anomaly at epoch: | 87.6751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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