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 59427U 26145.39303096 +.00000000 +00000-0 +71308-4 0 00004
2 59427 53.1613 285.3623 0001321 88.3094 271.8058 15.30198163 04
| Epoch (UTC): | 25 May 2026 09:25:57 |
| Eccentricity: | 0.0001321 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 285.3623° |
| argument of perigee: | 88.3094° |
| revolutions per day: | 15.30198163 |
| mean anomaly at epoch: | 271.8058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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