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 24298U 96051B 24277.15296700 .00000088 00000-0 74019-4 0 9999
2 24298 70.7926 200.6658 0015728 193.6656 166.4040 14.12455225448125
| Epoch (UTC): | 03 October 2024 03:40:16 |
| Eccentricity: | 0.0015728 |
| inclination: | 70.7926° |
| perigee height: | 839 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 200.6658° |
| argument of perigee: | 193.6656° |
| revolutions per day: | 14.12455225 |
| mean anomaly at epoch: | 166.4040° |
| orbit number at epoch: | 44812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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