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 00085U 61004C 23036.57677610 .00015835 00000-0 29855-2 0 9990
2 00085 38.7649 122.4339 0358350 110.3574 253.6046 14.30277332 68429
| Epoch (UTC): | 05 February 2023 13:50:33 |
| Eccentricity: | 0.0358350 |
| inclination: | 38.7649° |
| perigee height: | 534 km |
| apogee height: | 1048 km |
| right ascension of ascending node: | 122.4339° |
| argument of perigee: | 110.3574° |
| revolutions per day: | 14.30277332 |
| mean anomaly at epoch: | 253.6046° |
| orbit number at epoch: | 6842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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