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 04679U 70025BC 22181.51817198 .00000040 00000-0 10579-3 0 9993
2 04679 100.0708 274.1692 0017167 245.5612 182.5022 13.66703907592336
| Epoch (UTC): | 30 June 2022 12:26:10 |
| Eccentricity: | 0.0017167 |
| inclination: | 100.0708° |
| perigee height: | 999 km |
| apogee height: | 1024 km |
| right ascension of ascending node: | 274.1692° |
| argument of perigee: | 245.5612° |
| revolutions per day: | 13.66703907 |
| mean anomaly at epoch: | 182.5022° |
| orbit number at epoch: | 59233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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