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 00085U 61004C 21101.80788398 -.00001152 00000-0 -21663-3 0 9992
2 00085 38.7789 297.6580 0389366 328.5793 29.2219 14.21639631973556
| Epoch (UTC): | 11 April 2021 19:23:21 |
| Eccentricity: | 0.0389366 |
| inclination: | 38.7789° |
| perigee height: | 539 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 297.6580° |
| argument of perigee: | 328.5793° |
| revolutions per day: | 14.21639631 |
| mean anomaly at epoch: | 29.2219° |
| orbit number at epoch: | 97355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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