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 41557U 16033B 22180.18091791 .00009719 00000-0 28858-3 0 9994
2 41557 97.3890 277.8991 0009817 343.2260 104.9338 15.34951481339181
| Epoch (UTC): | 29 June 2022 04:20:31 |
| Eccentricity: | 0.0009817 |
| inclination: | 97.3890° |
| perigee height: | 454 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 277.8991° |
| argument of perigee: | 343.2260° |
| revolutions per day: | 15.34951481 |
| mean anomaly at epoch: | 104.9338° |
| orbit number at epoch: | 33918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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