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 54701U 22169C 24357.75140213 .00000759 00000-0 22199-3 0 9998
2 54701 59.9554 140.5117 0080199 320.9802 38.5473 14.50929830107522
| Epoch (UTC): | 22 December 2024 18:02:01 |
| Eccentricity: | 0.0080199 |
| inclination: | 59.9554° |
| perigee height: | 665 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 140.5117° |
| argument of perigee: | 320.9802° |
| revolutions per day: | 14.50929830 |
| mean anomaly at epoch: | 38.5473° |
| orbit number at epoch: | 10752 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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