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 30169U 99025UA 24280.70070924 .00050462 00000-0 99767-2 0 9996
2 30169 98.3797 346.4170 0262747 111.5413 11.6129 14.42511487914576
| Epoch (UTC): | 06 October 2024 16:49:01 |
| Eccentricity: | 0.0262747 |
| inclination: | 98.3797° |
| perigee height: | 563 km |
| apogee height: | 937 km |
| right ascension of ascending node: | 346.4170° |
| argument of perigee: | 111.5413° |
| revolutions per day: | 14.42511487 |
| mean anomaly at epoch: | 11.6129° |
| orbit number at epoch: | 91457 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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