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 59464U 26145.52672083 +.00000000 +00000-0 +47355-4 0 00000
2 59464 43.0015 320.6078 0001082 272.0711 88.0016 15.27577755 04
| Epoch (UTC): | 25 May 2026 12:38:28 |
| Eccentricity: | 0.0001082 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.6078° |
| argument of perigee: | 272.0711° |
| revolutions per day: | 15.27577755 |
| mean anomaly at epoch: | 88.0016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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