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 23091.17577873 .00009266 00000-0 44878-3 0 9997
2 40908 97.5275 94.5035 0016288 97.1203 333.8781 15.18656668416108
| Epoch (UTC): | 01 April 2023 04:13:07 |
| Eccentricity: | 0.0016288 |
| inclination: | 97.5275° |
| perigee height: | 498 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 94.5035° |
| argument of perigee: | 97.1203° |
| revolutions per day: | 15.18656668 |
| mean anomaly at epoch: | 333.8781° |
| orbit number at epoch: | 41610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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