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 23341.29392026 .00015032 00000-0 23020-2 0 9990
2 00085 38.7497 323.4410 0288653 41.2252 320.9922 14.48983594112318
| Epoch (UTC): | 07 December 2023 07:03:14 |
| Eccentricity: | 0.0288653 |
| inclination: | 38.7497° |
| perigee height: | 524 km |
| apogee height: | 934 km |
| right ascension of ascending node: | 323.4410° |
| argument of perigee: | 41.2252° |
| revolutions per day: | 14.48983594 |
| mean anomaly at epoch: | 320.9922° |
| orbit number at epoch: | 11231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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