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 28932U 06002B 24358.16844434 .00012977 00000-0 84442-3 0 9999
2 28932 98.2016 101.1173 0062952 294.4035 65.0629 15.06467436 27837
| Epoch (UTC): | 23 December 2024 04:02:33 |
| Eccentricity: | 0.0062952 |
| inclination: | 98.2016° |
| perigee height: | 503 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 101.1173° |
| argument of perigee: | 294.4035° |
| revolutions per day: | 15.06467436 |
| mean anomaly at epoch: | 65.0629° |
| orbit number at epoch: | 2783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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