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 47500U 21006CR 22331.95008489 .00004968 00000-0 23680-3 0 9998
2 47500 97.4269 28.5112 0011247 70.9750 289.2702 15.19507621102063
| Epoch (UTC): | 27 November 2022 22:48:07 |
| Eccentricity: | 0.0011247 |
| inclination: | 97.4269° |
| perigee height: | 499 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 28.5112° |
| argument of perigee: | 70.9750° |
| revolutions per day: | 15.19507621 |
| mean anomaly at epoch: | 289.2702° |
| orbit number at epoch: | 10206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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