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 59036U 26145.21295619 +.00000000 +00000-0 +36315-5 0 00002
2 59036 43.0005 217.0544 0001891 273.8539 86.2096 15.27573293 01
| Epoch (UTC): | 25 May 2026 05:06:39 |
| Eccentricity: | 0.0001891 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 217.0544° |
| argument of perigee: | 273.8539° |
| revolutions per day: | 15.27573293 |
| mean anomaly at epoch: | 86.2096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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