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 25198.87012312 .00003030 00000-0 13218-3 0 9990
2 13403 81.1480 109.6647 0024928 237.7890 122.0925 15.21580121341958
| Epoch (UTC): | 17 July 2025 20:52:58 |
| Eccentricity: | 0.0024928 |
| inclination: | 81.1480° |
| perigee height: | 484 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 109.6647° |
| argument of perigee: | 237.7890° |
| revolutions per day: | 15.21580121 |
| mean anomaly at epoch: | 122.0925° |
| orbit number at epoch: | 34195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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