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 22176.84466038 .00000077 00000-0 15076-3 0 9993
2 04679 100.0704 269.3101 0016961 257.9009 227.6474 13.66703098591692
| Epoch (UTC): | 25 June 2022 20:16:18 |
| Eccentricity: | 0.0016961 |
| inclination: | 100.0704° |
| perigee height: | 999 km |
| apogee height: | 1024 km |
| right ascension of ascending node: | 269.3101° |
| argument of perigee: | 257.9009° |
| revolutions per day: | 13.66703098 |
| mean anomaly at epoch: | 227.6474° |
| orbit number at epoch: | 59169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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