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 30284U 99025YV 24357.66809007 .00005883 00000-0 25083-2 0 9993
2 30284 98.7454 60.7349 0039066 62.3706 89.0839 14.25044602924519
| Epoch (UTC): | 22 December 2024 16:02:02 |
| Eccentricity: | 0.0039066 |
| inclination: | 98.7454° |
| perigee height: | 780 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 60.7349° |
| argument of perigee: | 62.3706° |
| revolutions per day: | 14.25044602 |
| mean anomaly at epoch: | 89.0839° |
| orbit number at epoch: | 92451 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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