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 57735U 26145.34482824 +.00000000 +00000-0 +64419-4 0 00001
2 57735 43.0058 106.8823 0001238 269.3523 90.7186 15.26743429 05
| Epoch (UTC): | 25 May 2026 08:16:33 |
| Eccentricity: | 0.0001238 |
| inclination: | 43.0058° |
| perigee height: | 485 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 106.8823° |
| argument of perigee: | 269.3523° |
| revolutions per day: | 15.26743429 |
| mean anomaly at epoch: | 90.7186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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