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 09841U 77012A 23088.87114503 -.00000012 00000-0 72773-4 0 9993
2 09841 65.7571 140.0996 1735044 231.9589 111.1927 10.73847559807506
| Epoch (UTC): | 29 March 2023 20:54:26 |
| Eccentricity: | 0.1735044 |
| inclination: | 65.7571° |
| perigee height: | 794 km |
| apogee height: | 3806 km |
| right ascension of ascending node: | 140.0996° |
| argument of perigee: | 231.9589° |
| revolutions per day: | 10.73847559 |
| mean anomaly at epoch: | 111.1927° |
| orbit number at epoch: | 80750 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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