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 59013U 26145.20867419 +.00000000 +00000-0 +12372-3 0 00004
2 59013 53.1609 83.0550 0001264 102.5670 257.5473 15.30174813 05
| Epoch (UTC): | 25 May 2026 05:00:29 |
| Eccentricity: | 0.0001264 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 83.0550° |
| argument of perigee: | 102.5670° |
| revolutions per day: | 15.30174813 |
| mean anomaly at epoch: | 257.5473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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