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 59265U 26145.48495583 +.00000000 +00000-0 +21663-4 0 00006
2 59265 53.1595 184.4721 0001087 89.5761 270.5364 15.30190578 02
| Epoch (UTC): | 25 May 2026 11:38:20 |
| Eccentricity: | 0.0001087 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.4721° |
| argument of perigee: | 89.5761° |
| revolutions per day: | 15.30190578 |
| mean anomaly at epoch: | 270.5364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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