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 59798U 26145.33960302 +.00000000 +00000-0 +13081-4 0 00002
2 59798 42.9995 136.3928 0001165 272.3890 87.6828 15.27575510 01
| Epoch (UTC): | 25 May 2026 08:09:01 |
| Eccentricity: | 0.0001165 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 136.3928° |
| argument of perigee: | 272.3890° |
| revolutions per day: | 15.27575510 |
| mean anomaly at epoch: | 87.6828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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