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 00573U 26046.25915873 +.00000000 +00000-0 +16999-3 0 00003
2 00573 42.7467 113.1599 4008258 2.5659 17.4402 6.39265311 04
| Epoch (UTC): | 15 February 2026 06:13:11 |
| Eccentricity: | 0.4008258 |
| inclination: | 42.7467° |
| perigee height: | 970 km |
| apogee height: | 10801 km |
| right ascension of ascending node: | 113.1599° |
| argument of perigee: | 2.5659° |
| revolutions per day: | 6.39265311 |
| mean anomaly at epoch: | 17.4402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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