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 29507U 06046C 20021.65363195 .00000089 00000-0 11981-4 0 9993
2 29507 97.7461 43.9779 0047051 305.4215 54.2619 15.00470165723250
| Epoch (UTC): | 21 January 2020 15:41:13 |
| Eccentricity: | 0.0047051 |
| inclination: | 97.7461° |
| perigee height: | 533 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 43.9779° |
| argument of perigee: | 305.4215° |
| revolutions per day: | 15.00470165 |
| mean anomaly at epoch: | 54.2619° |
| orbit number at epoch: | 72325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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