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 40907U 15049J 23087.98541140 .00022752 00000-0 89065-3 0 9990
2 40907 97.4962 95.3080 0013772 80.8489 330.9912 15.25733271416241
| Epoch (UTC): | 28 March 2023 23:38:59 |
| Eccentricity: | 0.0013772 |
| inclination: | 97.4962° |
| perigee height: | 479 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 95.3080° |
| argument of perigee: | 80.8489° |
| revolutions per day: | 15.25733271 |
| mean anomaly at epoch: | 330.9912° |
| orbit number at epoch: | 41624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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