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 20328U 89089D 24280.80498390 .00000382 00000-0 26702-3 0 9999
2 20328 98.9194 284.5354 0003449 49.6568 123.6305 14.04429015786300
| Epoch (UTC): | 06 October 2024 19:19:10 |
| Eccentricity: | 0.0003449 |
| inclination: | 98.9194° |
| perigee height: | 876 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 284.5354° |
| argument of perigee: | 49.6568° |
| revolutions per day: | 14.04429015 |
| mean anomaly at epoch: | 123.6305° |
| orbit number at epoch: | 78630 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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