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 29944U 99025JS 24358.18231149 .00016228 00000-0 16427-2 0 9995
2 29944 99.0143 241.6590 0192314 273.4770 211.3408 14.78258194952153
| Epoch (UTC): | 23 December 2024 04:22:31 |
| Eccentricity: | 0.0192314 |
| inclination: | 99.0143° |
| perigee height: | 500 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 241.6590° |
| argument of perigee: | 273.4770° |
| revolutions per day: | 14.78258194 |
| mean anomaly at epoch: | 211.3408° |
| orbit number at epoch: | 95215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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