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 59803U 26145.46394916 +.00000000 +00000-0 +27837-4 0 00009
2 59803 43.0014 135.6034 0001251 271.0659 89.0050 15.27579914 02
| Epoch (UTC): | 25 May 2026 11:08:05 |
| Eccentricity: | 0.0001251 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.6034° |
| argument of perigee: | 271.0659° |
| revolutions per day: | 15.27579914 |
| mean anomaly at epoch: | 89.0050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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