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 21419U 91041B 24282.57303237 .00001787 00000-0 63367-3 0 9991
2 21419 74.0377 93.6155 0039602 89.1328 271.4361 14.34759410743261
| Epoch (UTC): | 08 October 2024 13:45:09 |
| Eccentricity: | 0.0039602 |
| inclination: | 74.0377° |
| perigee height: | 747 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 93.6155° |
| argument of perigee: | 89.1328° |
| revolutions per day: | 14.34759410 |
| mean anomaly at epoch: | 271.4361° |
| orbit number at epoch: | 74326 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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