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 12849U 81094B 25188.52658209 .00001794 00000-0 15828-3 0 9995
2 12849 82.4916 62.6265 0875140 42.7425 323.8491 13.56975844139467
| Epoch (UTC): | 07 July 2025 12:38:16 |
| Eccentricity: | 0.0875140 |
| inclination: | 82.4916° |
| perigee height: | 397 km |
| apogee height: | 1696 km |
| right ascension of ascending node: | 62.6265° |
| argument of perigee: | 42.7425° |
| revolutions per day: | 13.56975844 |
| mean anomaly at epoch: | 323.8491° |
| orbit number at epoch: | 13946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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