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 2940U 67080B 24358.16580238 .00000314 00000-0 17606-3 0 9992
2 2940 98.5511 194.8168 0036924 327.6354 32.2557 14.17013324958762
| Epoch (UTC): | 23 December 2024 03:58:45 |
| Eccentricity: | 0.0036924 |
| inclination: | 98.5511° |
| perigee height: | 809 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 194.8168° |
| argument of perigee: | 327.6354° |
| revolutions per day: | 14.17013324 |
| mean anomaly at epoch: | 32.2557° |
| orbit number at epoch: | 95876 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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