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 12585U 81065A 22147.91692976 .00005000 00000-0 20873-3 0 9994
2 12585 97.5831 152.5560 0012757 201.2103 158.8606 15.24052948231045
| Epoch (UTC): | 27 May 2022 22:00:22 |
| Eccentricity: | 0.0012757 |
| inclination: | 97.5831° |
| perigee height: | 485 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 152.5560° |
| argument of perigee: | 201.2103° |
| revolutions per day: | 15.24052948 |
| mean anomaly at epoch: | 158.8606° |
| orbit number at epoch: | 23104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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