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 80000U 91056 21045.33426173 .00000012 00000-0 00000-0 0 9993
2 80000 82.5515 74.2588 0023199 283.7724 76.0921 13.20138489 663
| Epoch (UTC): | 14 February 2021 08:01:20 |
| Eccentricity: | 0.0023199 |
| inclination: | 82.5515° |
| perigee height: | 1166 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 74.2588° |
| argument of perigee: | 283.7724° |
| revolutions per day: | 13.20138489 |
| mean anomaly at epoch: | 76.0921° |
| orbit number at epoch: | 66 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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