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 23079.20183122 .00007883 00000-0 14917-2 0 9994
2 00085 38.7632 261.2044 0346042 39.1100 323.4132 14.32382068 74530
| Epoch (UTC): | 20 March 2023 04:50:38 |
| Eccentricity: | 0.0346042 |
| inclination: | 38.7632° |
| perigee height: | 536 km |
| apogee height: | 1031 km |
| right ascension of ascending node: | 261.2044° |
| argument of perigee: | 39.1100° |
| revolutions per day: | 14.32382068 |
| mean anomaly at epoch: | 323.4132° |
| orbit number at epoch: | 7453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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