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 24252.13419414 .00023211 00000-0 82978-3 0 9998
2 40908 97.5248 261.5678 0013568 65.2906 294.9744 15.28734327496150
| Epoch (UTC): | 08 September 2024 03:13:14 |
| Eccentricity: | 0.0013568 |
| inclination: | 97.5248° |
| perigee height: | 470 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 261.5678° |
| argument of perigee: | 65.2906° |
| revolutions per day: | 15.28734327 |
| mean anomaly at epoch: | 294.9744° |
| orbit number at epoch: | 49615 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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