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 57700U 26145.12176411 +.00000000 +00000-0 +74549-4 0 00006
2 57700 43.0033 53.7556 0001601 251.7436 108.3242 15.27589490 01
| Epoch (UTC): | 25 May 2026 02:55:20 |
| Eccentricity: | 0.0001601 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 53.7556° |
| argument of perigee: | 251.7436° |
| revolutions per day: | 15.27589490 |
| mean anomaly at epoch: | 108.3242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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