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 59673U 26145.51553323 +.00000000 +00000-0 +51988-4 0 00003
2 59673 43.0005 327.8339 0001941 264.0289 96.0341 15.27578272 04
| Epoch (UTC): | 25 May 2026 12:22:22 |
| Eccentricity: | 0.0001941 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.8339° |
| argument of perigee: | 264.0289° |
| revolutions per day: | 15.27578272 |
| mean anomaly at epoch: | 96.0341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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