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 35937U 09052A 23073.10695184 0.00000000 00000-0 00000-0 0 05
2 35937 57.9871 106.1767 0004237 0.1135 359.9672 12.83498841 09
| Epoch (UTC): | 14 March 2023 02:34:00 |
| Eccentricity: | 0.0004237 |
| inclination: | 57.9871° |
| perigee height: | 1324 km |
| apogee height: | 1330 km |
| right ascension of ascending node: | 106.1767° |
| argument of perigee: | 0.1135° |
| revolutions per day: | 12.83498841 |
| mean anomaly at epoch: | 359.9672° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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