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 12298U 81013B 24277.20805855 .00000202 00000-0 18890-3 0 9993
2 12298 82.9499 150.8038 0029799 356.6314 124.5760 13.76831884191885
| Epoch (UTC): | 03 October 2024 04:59:36 |
| Eccentricity: | 0.0029799 |
| inclination: | 82.9499° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 150.8038° |
| argument of perigee: | 356.6314° |
| revolutions per day: | 13.76831884 |
| mean anomaly at epoch: | 124.5760° |
| orbit number at epoch: | 19188 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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