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 21805U 91080B 23080.23451966 -.00000266 00000-0 00000-0 0 9998
2 21805 14.6436 354.1469 0008067 76.6510 146.9903 0.99187599 13968
| Epoch (UTC): | 21 March 2023 05:37:42 |
| Eccentricity: | 0.0008067 |
| inclination: | 14.6436° |
| perigee height: | 36058 km |
| apogee height: | 36127 km |
| right ascension of ascending node: | 354.1469° |
| argument of perigee: | 76.6510° |
| revolutions per day: | 0.99187599 |
| mean anomaly at epoch: | 146.9903° |
| orbit number at epoch: | 1396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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