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 20692U 90050D 23124.12128172 0.00008100 00000-0 78655-3 0 05
2 20692 63.3028 8.2124 0917255 63.5636 296.4364 13.46269193 06
| Epoch (UTC): | 04 May 2023 02:54:38 |
| Eccentricity: | 0.0917255 |
| inclination: | 63.3028° |
| perigee height: | 401 km |
| apogee height: | 1770 km |
| right ascension of ascending node: | 8.2124° |
| argument of perigee: | 63.5636° |
| revolutions per day: | 13.46269193 |
| mean anomaly at epoch: | 296.4364° |
| 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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