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 59527U 26145.26574119 +.00000000 +00000-0 +12848-3 0 00000
2 59527 43.0022 245.8416 0001700 271.6027 88.4630 15.27572383 06
| Epoch (UTC): | 25 May 2026 06:22:40 |
| Eccentricity: | 0.0001700 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.8416° |
| argument of perigee: | 271.6027° |
| revolutions per day: | 15.27572383 |
| mean anomaly at epoch: | 88.4630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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