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 30462U 99025AFZ 24356.99361243 .00000791 00000-0 46628-3 0 9993
2 30462 98.7912 348.9763 0140568 169.1030 257.7548 14.05846346917946
| Epoch (UTC): | 21 December 2024 23:50:48 |
| Eccentricity: | 0.0140568 |
| inclination: | 98.7912° |
| perigee height: | 771 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 348.9763° |
| argument of perigee: | 169.1030° |
| revolutions per day: | 14.05846346 |
| mean anomaly at epoch: | 257.7548° |
| orbit number at epoch: | 91794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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