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 115U 60002D 22221.36941122 .00000915 00000-0 13295-3 0 9990
2 115 48.1660 107.7870 0033505 100.7993 259.6694 14.84513698329249
| Epoch (UTC): | 09 August 2022 08:51:57 |
| Eccentricity: | 0.0033505 |
| inclination: | 48.1660° |
| perigee height: | 591 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 107.7870° |
| argument of perigee: | 100.7993° |
| revolutions per day: | 14.84513698 |
| mean anomaly at epoch: | 259.6694° |
| orbit number at epoch: | 32924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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