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 23344.25760902 .00011816 00000-0 18128-2 0 9990
2 00085 38.7489 307.6247 0288307 61.9446 301.0149 14.49063438112746
| Epoch (UTC): | 10 December 2023 06:10:57 |
| Eccentricity: | 0.0288307 |
| inclination: | 38.7489° |
| perigee height: | 524 km |
| apogee height: | 933 km |
| right ascension of ascending node: | 307.6247° |
| argument of perigee: | 61.9446° |
| revolutions per day: | 14.49063438 |
| mean anomaly at epoch: | 301.0149° |
| orbit number at epoch: | 11274 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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