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 00107U 61013A 24280.21560440 .00006348 00000-0 79070-3 0 9994
2 00107 28.7856 273.1620 0515346 127.3070 237.5616 14.16853000188444
| Epoch (UTC): | 06 October 2024 05:10:28 |
| Eccentricity: | 0.0515346 |
| inclination: | 28.7856° |
| perigee height: | 464 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 273.1620° |
| argument of perigee: | 127.3070° |
| revolutions per day: | 14.16853000 |
| mean anomaly at epoch: | 237.5616° |
| orbit number at epoch: | 18844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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