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 15944U 85069A 23271.91304828 .00012164 00000-0 41121-3 0 9997
2 15944 82.4990 107.1188 0014728 39.6019 320.6294 15.30403177 86543
| Epoch (UTC): | 28 September 2023 21:54:47 |
| Eccentricity: | 0.0014728 |
| inclination: | 82.4990° |
| perigee height: | 464 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 107.1188° |
| argument of perigee: | 39.6019° |
| revolutions per day: | 15.30403177 |
| mean anomaly at epoch: | 320.6294° |
| orbit number at epoch: | 8654 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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