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 19650U 88102B 24260.16198420 .00000316 00000-0 18426-3 0 9999
2 19650 70.9995 206.6075 0012126 116.2202 244.0169 14.16012653850798
| Epoch (UTC): | 16 September 2024 03:53:15 |
| Eccentricity: | 0.0012126 |
| inclination: | 70.9995° |
| perigee height: | 830 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 206.6075° |
| argument of perigee: | 116.2202° |
| revolutions per day: | 14.16012653 |
| mean anomaly at epoch: | 244.0169° |
| orbit number at epoch: | 85079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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