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 data is extracted from the following two-line orbital elements,
1 13403U 82079B 25198.54131452 .00003148 00000-0 13735-3 0 9995
2 13403 81.1480 110.0511 0024910 238.9774 120.9012 15.21577962341907
| Epoch (UTC): | 17 July 2025 12:59:29 |
| Eccentricity: | 0.0024910 |
| inclination: | 81.1480° |
| perigee height: | 484 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 110.0511° |
| argument of perigee: | 238.9774° |
| revolutions per day: | 15.21577962 |
| mean anomaly at epoch: | 120.9012° |
| orbit number at epoch: | 34190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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