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 57397U 18081Q 24355.88886701 .00002850 00000-0 77345-3 0 9998
2 57397 99.4057 221.8321 0202130 20.6097 340.3095 14.37130162 88871
| Epoch (UTC): | 20 December 2024 21:19:58 |
| Eccentricity: | 0.0202130 |
| inclination: | 99.4057° |
| perigee height: | 623 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 221.8321° |
| argument of perigee: | 20.6097° |
| revolutions per day: | 14.37130162 |
| mean anomaly at epoch: | 340.3095° |
| orbit number at epoch: | 8887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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