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 59795U 26145.44211544 +.00000000 +00000-0 +98172-4 0 00002
2 59795 43.0012 135.4399 0000922 252.2479 107.8272 15.27550065 08
| Epoch (UTC): | 25 May 2026 10:36:38 |
| Eccentricity: | 0.0000922 |
| inclination: | 43.0012° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.4399° |
| argument of perigee: | 252.2479° |
| revolutions per day: | 15.27550065 |
| mean anomaly at epoch: | 107.8272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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