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 00050U 60009B 24256.60643724 -.00000035 00000-0 46721-3 0 9993
2 00050 47.2350 356.2408 0113725 259.4890 99.3069 12.20144829859249
| Epoch (UTC): | 12 September 2024 14:33:16 |
| Eccentricity: | 0.0113725 |
| inclination: | 47.2350° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 356.2408° |
| argument of perigee: | 259.4890° |
| revolutions per day: | 12.20144829 |
| mean anomaly at epoch: | 99.3069° |
| orbit number at epoch: | 85924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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