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 23335.21924654 .00009311 00000-0 96099-3 0 9999
2 40074 98.3380 248.5963 0004718 24.0433 336.1003 14.90413942509110
| Epoch (UTC): | 01 December 2023 05:15:42 |
| Eccentricity: | 0.0004718 |
| inclination: | 98.3380° |
| perigee height: | 593 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 248.5963° |
| argument of perigee: | 24.0433° |
| revolutions per day: | 14.90413942 |
| mean anomaly at epoch: | 336.1003° |
| orbit number at epoch: | 50911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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