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 15543U 85010B 25189.43178464 .00000053 00000-0 00000-0 0 9992
2 15543 13.2961 316.8257 0126584 48.0700 134.7136 0.99807026 4391
| Epoch (UTC): | 08 July 2025 10:21:46 |
| Eccentricity: | 0.0126584 |
| inclination: | 13.2961° |
| perigee height: | 35381 km |
| apogee height: | 36452 km |
| right ascension of ascending node: | 316.8257° |
| argument of perigee: | 48.0700° |
| revolutions per day: | 0.99807026 |
| mean anomaly at epoch: | 134.7136° |
| orbit number at epoch: | 439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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