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 40908U 15049K 23090.52196302 .00009097 00000-0 44084-3 0 9990
2 40908 97.5274 93.8525 0016328 99.4011 359.3634 15.18643370416005
| Epoch (UTC): | 31 March 2023 12:31:37 |
| Eccentricity: | 0.0016328 |
| inclination: | 97.5274° |
| perigee height: | 498 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 93.8525° |
| argument of perigee: | 99.4011° |
| revolutions per day: | 15.18643370 |
| mean anomaly at epoch: | 359.3634° |
| orbit number at epoch: | 41600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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