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 20U 59007A 21334.62695963 .00000786 00000-0 31021-3 0 9993
2 20 33.3484 89.4956 1664749 204.8661 146.1805 11.55918335292104
| Epoch (UTC): | 30 November 2021 15:02:49 |
| Eccentricity: | 0.1664749 |
| inclination: | 33.3484° |
| perigee height: | 509 km |
| apogee height: | 3260 km |
| right ascension of ascending node: | 89.4956° |
| argument of perigee: | 204.8661° |
| revolutions per day: | 11.55918335 |
| mean anomaly at epoch: | 146.1805° |
| orbit number at epoch: | 29210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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