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 40900U 15049B 22277.00876255 .00043480 00000-0 10373-2 0 9990
2 40900 97.3969 295.9231 0005762 243.5718 177.4567 15.41409178391302
| Epoch (UTC): | 04 October 2022 00:12:37 |
| Eccentricity: | 0.0005762 |
| inclination: | 97.3969° |
| perigee height: | 438 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 295.9231° |
| argument of perigee: | 243.5718° |
| revolutions per day: | 15.41409178 |
| mean anomaly at epoch: | 177.4567° |
| orbit number at epoch: | 39130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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