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 00020U 59007A 21333.41786920 .00000802 00000-0 31794-3 0 9999
2 00020 33.3470 93.8045 1664669 198.4494 154.7903 11.55916741291933
| Epoch (UTC): | 29 November 2021 10:01:43 |
| Eccentricity: | 0.1664669 |
| inclination: | 33.3470° |
| perigee height: | 509 km |
| apogee height: | 3260 km |
| right ascension of ascending node: | 93.8045° |
| argument of perigee: | 198.4494° |
| revolutions per day: | 11.55916741 |
| mean anomaly at epoch: | 154.7903° |
| orbit number at epoch: | 29193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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