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 20963U 90097B 22058.65362887 0.00000000 00000-0 00000-0 0 00
2 20963 15.6557 347.2999 0011711 240.1320 119.7636 0.98581418 04
| Epoch (UTC): | 27 February 2022 15:41:13 |
| Eccentricity: | 0.0011711 |
| inclination: | 15.6557° |
| perigee height: | 36217 km |
| apogee height: | 36317 km |
| right ascension of ascending node: | 347.2999° |
| argument of perigee: | 240.1320° |
| revolutions per day: | 0.98581418 |
| mean anomaly at epoch: | 119.7636° |
| 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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