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 23716U 95062B 23031.08142075 -.00000097 00000-0 10262-2 0 9997
2 23716 5.1968 323.1501 8366503 289.3056 5.0104 0.95000312 94495
| Epoch (UTC): | 31 January 2023 01:57:14 |
| Eccentricity: | 0.8366503 |
| inclination: | 5.1968° |
| perigee height: | 762 km |
| apogee height: | 73902 km |
| right ascension of ascending node: | 323.1501° |
| argument of perigee: | 289.3056° |
| revolutions per day: | 0.95000312 |
| mean anomaly at epoch: | 5.0104° |
| orbit number at epoch: | 9449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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