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 22179.39214139 .00003052 00000-0 61206-3 0 9995
2 00085 38.7646 190.0960 0371575 52.8179 310.5896 14.26997209 36644
| Epoch (UTC): | 28 June 2022 09:24:41 |
| Eccentricity: | 0.0371575 |
| inclination: | 38.7646° |
| perigee height: | 535 km |
| apogee height: | 1068 km |
| right ascension of ascending node: | 190.0960° |
| argument of perigee: | 52.8179° |
| revolutions per day: | 14.26997209 |
| mean anomaly at epoch: | 310.5896° |
| orbit number at epoch: | 3664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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