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 60954U 98067WU 24334.01561250 .09108413 12187-4 11947-2 0 9993
2 60954 51.6047 205.2539 0008835 243.5267 116.4851 16.34683424 14392
| Epoch (UTC): | 29 November 2024 00:22:28 |
| Eccentricity: | 0.0008835 |
| inclination: | 51.6047° |
| perigee height: | 174 km |
| apogee height: | 186 km |
| right ascension of ascending node: | 205.2539° |
| argument of perigee: | 243.5267° |
| revolutions per day: | 16.34683424 |
| mean anomaly at epoch: | 116.4851° |
| orbit number at epoch: | 1439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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