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 25133.55815572 .00005070 00000-0 22488-3 0 9998
2 13403 81.1482 186.3665 0027923 99.6193 260.8195 15.21042527332022
| Epoch (UTC): | 13 May 2025 13:23:44 |
| Eccentricity: | 0.0027923 |
| inclination: | 81.1482° |
| perigee height: | 483 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 186.3665° |
| argument of perigee: | 99.6193° |
| revolutions per day: | 15.21042527 |
| mean anomaly at epoch: | 260.8195° |
| orbit number at epoch: | 33202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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