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 41603U 16040E 21023.76477238 .00000049 00000-0 53651-5 0 9995
2 41603 97.2797 76.0105 0014202 144.2124 325.9150 15.19947458254608
| Epoch (UTC): | 23 January 2021 18:21:16 |
| Eccentricity: | 0.0014202 |
| inclination: | 97.2797° |
| perigee height: | 496 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 76.0105° |
| argument of perigee: | 144.2124° |
| revolutions per day: | 15.19947458 |
| mean anomaly at epoch: | 325.9150° |
| orbit number at epoch: | 25460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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