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 21056.70949869 .00002114 00000-0 45196-3 0 9996
2 00085 38.7762 168.0727 0392868 28.0198 334.1115 14.21647360967131
| Epoch (UTC): | 25 February 2021 17:01:40 |
| Eccentricity: | 0.0392868 |
| inclination: | 38.7762° |
| perigee height: | 537 km |
| apogee height: | 1102 km |
| right ascension of ascending node: | 168.0727° |
| argument of perigee: | 28.0198° |
| revolutions per day: | 14.21647360 |
| mean anomaly at epoch: | 334.1115° |
| orbit number at epoch: | 96713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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