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 50463U 21130A 21362.00000000 .00000000 00000-0 00000-0 0 9999
2 50463 4.6198 89.0659 9884983 192.3200 17.4027 0.01958082 27
| Epoch (UTC): | 28 December 2021 00:00:00 |
| Eccentricity: | 0.9884983 |
| inclination: | 4.6198° |
| perigee height: | 309 km |
| apogee height: | 1149825 km |
| right ascension of ascending node: | 89.0659° |
| argument of perigee: | 192.3200° |
| revolutions per day: | 0.01958082 |
| mean anomaly at epoch: | 17.4027° |
| orbit number at epoch: | 2 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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