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 12889U 81100C 24278.89527437 .00002282 00000-0 11225-2 0 9993
2 12889 99.8733 252.9485 1311598 83.8058 337.2804 12.19221353905712
| Epoch (UTC): | 04 October 2024 21:29:11 |
| Eccentricity: | 0.1311598 |
| inclination: | 99.8733° |
| perigee height: | 550 km |
| apogee height: | 2642 km |
| right ascension of ascending node: | 252.9485° |
| argument of perigee: | 83.8058° |
| revolutions per day: | 12.19221353 |
| mean anomaly at epoch: | 337.2804° |
| orbit number at epoch: | 90571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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