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 59148U 26145.68114726 +.00000000 +00000-0 +83875-3 0 00007
2 59148 97.5423 293.3878 0005716 255.1235 104.9383 15.48997534 04
| Epoch (UTC): | 25 May 2026 16:20:51 |
| Eccentricity: | 0.0005716 |
| inclination: | 97.5423° |
| perigee height: | 416 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 293.3878° |
| argument of perigee: | 255.1235° |
| revolutions per day: | 15.48997534 |
| mean anomaly at epoch: | 104.9383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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