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 59501U 26145.36421346 +.00000000 +00000-0 -28037-4 0 00005
2 59501 42.9982 266.5820 0000493 282.0283 78.0514 15.27582116 09
| Epoch (UTC): | 25 May 2026 08:44:28 |
| Eccentricity: | 0.0000493 |
| inclination: | 42.9982° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 266.5820° |
| argument of perigee: | 282.0283° |
| revolutions per day: | 15.27582116 |
| mean anomaly at epoch: | 78.0514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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