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 59679U 26145.53394021 +.00000000 +00000-0 +31057-3 0 00003
2 59679 97.3293 221.5906 0028679 119.7835 240.6265 15.33342425 09
| Epoch (UTC): | 25 May 2026 12:48:52 |
| Eccentricity: | 0.0028679 |
| inclination: | 97.3293° |
| perigee height: | 446 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 221.5906° |
| argument of perigee: | 119.7835° |
| revolutions per day: | 15.33342425 |
| mean anomaly at epoch: | 240.6265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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