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 12964U 81053EK 24279.87342476 .00000177 00000-0 15419-3 0 9992
2 12964 82.9470 218.6996 0040251 78.9486 343.5323 13.80262648163383
| Epoch (UTC): | 05 October 2024 20:57:43 |
| Eccentricity: | 0.0040251 |
| inclination: | 82.9470° |
| perigee height: | 933 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 218.6996° |
| argument of perigee: | 78.9486° |
| revolutions per day: | 13.80262648 |
| mean anomaly at epoch: | 343.5323° |
| orbit number at epoch: | 16338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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