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 15483U 85006B 25193.89127521 .00000174 00000-0 66634-4 0 9996
2 15483 74.0470 342.3190 0019104 314.5276 207.9287 14.37608546119561
| Epoch (UTC): | 12 July 2025 21:23:26 |
| Eccentricity: | 0.0019104 |
| inclination: | 74.0470° |
| perigee height: | 753 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 342.3190° |
| argument of perigee: | 314.5276° |
| revolutions per day: | 14.37608546 |
| mean anomaly at epoch: | 207.9287° |
| orbit number at epoch: | 11956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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