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 13354U 82069B 25349.96756496 .00000049 00000-0 31811-4 0 9997
2 13354 82.9588 191.8813 0052768 51.6820 308.9065 13.79251921185150
| Epoch (UTC): | 15 December 2025 23:13:17 |
| Eccentricity: | 0.0052768 |
| inclination: | 82.9588° |
| perigee height: | 928 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 191.8813° |
| argument of perigee: | 51.6820° |
| revolutions per day: | 13.79251921 |
| mean anomaly at epoch: | 308.9065° |
| orbit number at epoch: | 18515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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