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 59077U 26145.63961983 +.00000000 +00000-0 +79814-4 0 00007
2 59077 43.0051 235.8303 0002330 282.4904 77.5687 15.27577943 04
| Epoch (UTC): | 25 May 2026 15:21:03 |
| Eccentricity: | 0.0002330 |
| inclination: | 43.0051° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 235.8303° |
| argument of perigee: | 282.4904° |
| revolutions per day: | 15.27577943 |
| mean anomaly at epoch: | 77.5687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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