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 59799U 26145.45624073 +.00000000 +00000-0 +55654-4 0 00000
2 59799 43.0008 135.5458 0001238 269.7024 90.3685 15.27593465 09
| Epoch (UTC): | 25 May 2026 10:56:59 |
| Eccentricity: | 0.0001238 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.5458° |
| argument of perigee: | 269.7024° |
| revolutions per day: | 15.27593465 |
| mean anomaly at epoch: | 90.3685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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