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 40021U 14033M 24340.57132032 .00029231 00000-0 14821-2 0 9999
2 40021 98.1004 334.4358 0008290 231.3073 128.7417 15.16879262570019
| Epoch (UTC): | 05 December 2024 13:42:42 |
| Eccentricity: | 0.0008290 |
| inclination: | 98.1004° |
| perigee height: | 509 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 334.4358° |
| argument of perigee: | 231.3073° |
| revolutions per day: | 15.16879262 |
| mean anomaly at epoch: | 128.7417° |
| orbit number at epoch: | 57001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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