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 40057U 14034E 23340.76381999 .00003753 00000-0 46134-3 0 9991
2 40057 98.3581 181.7319 0010593 50.4228 309.7918 14.83639181509006
| Epoch (UTC): | 06 December 2023 18:19:54 |
| Eccentricity: | 0.0010593 |
| inclination: | 98.3581° |
| perigee height: | 610 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 181.7319° |
| argument of perigee: | 50.4228° |
| revolutions per day: | 14.83639181 |
| mean anomaly at epoch: | 309.7918° |
| orbit number at epoch: | 50900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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