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 57776U 26145.38886799 +.00000000 +00000-0 +11679-3 0 00008
2 57776 43.0018 121.6145 0000856 242.9247 117.1517 15.27582420 08
| Epoch (UTC): | 25 May 2026 09:19:58 |
| Eccentricity: | 0.0000856 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.6145° |
| argument of perigee: | 242.9247° |
| revolutions per day: | 15.27582420 |
| mean anomaly at epoch: | 117.1517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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