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 57260U 26145.46695362 +.00000000 +00000-0 +34958-4 0 00005
2 57260 43.0030 306.1457 0001172 259.0529 101.0191 15.27577369 06
| Epoch (UTC): | 25 May 2026 11:12:24 |
| Eccentricity: | 0.0001172 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.1457° |
| argument of perigee: | 259.0529° |
| revolutions per day: | 15.27577369 |
| mean anomaly at epoch: | 101.0191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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