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 20442U 90005G 24260.93330625 .00000689 00000-0 26529-3 0 9991
2 20442 98.8907 253.6507 0010480 277.8974 82.1020 14.33662052810925
| Epoch (UTC): | 16 September 2024 22:23:57 |
| Eccentricity: | 0.0010480 |
| inclination: | 98.8907° |
| perigee height: | 772 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 253.6507° |
| argument of perigee: | 277.8974° |
| revolutions per day: | 14.33662052 |
| mean anomaly at epoch: | 82.1020° |
| orbit number at epoch: | 81092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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