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 02701U 65048E 22331.43249098 .00000255 00000-0 30899-3 0 9997
2 02701 89.9051 302.1977 0065245 123.0376 37.0368 13.62805951844505
| Epoch (UTC): | 27 November 2022 10:22:47 |
| Eccentricity: | 0.0065245 |
| inclination: | 89.9051° |
| perigee height: | 977 km |
| apogee height: | 1074 km |
| right ascension of ascending node: | 302.1977° |
| argument of perigee: | 123.0376° |
| revolutions per day: | 13.62805951 |
| mean anomaly at epoch: | 37.0368° |
| orbit number at epoch: | 84450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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