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 20894U 90081BE 24276.49899955 .00009809 00000-0 37074-2 0 9999
2 20894 98.5280 272.7295 0019159 353.6983 126.6895 14.31342782761155
| Epoch (UTC): | 02 October 2024 11:58:33 |
| Eccentricity: | 0.0019159 |
| inclination: | 98.5280° |
| perigee height: | 773 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 272.7295° |
| argument of perigee: | 353.6983° |
| revolutions per day: | 14.31342782 |
| mean anomaly at epoch: | 126.6895° |
| orbit number at epoch: | 76115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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