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 35319U 99057RX 24357.06730503 .00002177 00000-0 10101-2 0 9998
2 35319 98.6894 84.2790 0193903 90.9240 30.7766 14.12220679188433
| Epoch (UTC): | 22 December 2024 01:36:55 |
| Eccentricity: | 0.0193903 |
| inclination: | 98.6894° |
| perigee height: | 711 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 84.2790° |
| argument of perigee: | 90.9240° |
| revolutions per day: | 14.12220679 |
| mean anomaly at epoch: | 30.7766° |
| orbit number at epoch: | 18843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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