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 37465U 99025EJK 22220.74584217 .00003923 00000-0 10167-2 0 9990
2 37465 99.3625 47.3566 0045467 17.6769 342.5991 14.49851164409980
| Epoch (UTC): | 08 August 2022 17:54:00 |
| Eccentricity: | 0.0045467 |
| inclination: | 99.3625° |
| perigee height: | 694 km |
| apogee height: | 758 km |
| right ascension of ascending node: | 47.3566° |
| argument of perigee: | 17.6769° |
| revolutions per day: | 14.49851164 |
| mean anomaly at epoch: | 342.5991° |
| orbit number at epoch: | 40998 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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