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 20642U 90050E 23111.23159205 0.00011600 00000-0 10880-2 0 03
2 20642 63.2999 43.3261 0922661 61.0968 298.9031 13.46088457 07
| Epoch (UTC): | 21 April 2023 05:33:29 |
| Eccentricity: | 0.0922661 |
| inclination: | 63.2999° |
| perigee height: | 398 km |
| apogee height: | 1775 km |
| right ascension of ascending node: | 43.3261° |
| argument of perigee: | 61.0968° |
| revolutions per day: | 13.46088457 |
| mean anomaly at epoch: | 298.9031° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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