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 40074U 14037F 23339.71723344 .00006796 00000-0 70196-3 0 9995
2 40074 98.3383 253.3430 0004376 14.5865 345.5477 14.90492811509783
| Epoch (UTC): | 05 December 2023 17:12:48 |
| Eccentricity: | 0.0004376 |
| inclination: | 98.3383° |
| perigee height: | 593 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 253.3430° |
| argument of perigee: | 14.5865° |
| revolutions per day: | 14.90492811 |
| mean anomaly at epoch: | 345.5477° |
| orbit number at epoch: | 50978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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