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 48274U 21035A 24252.16307111 .00070440 00000-0 73511-3 0 9996
2 48274 41.4686 297.3488 0001497 52.7304 307.3672 15.63544329192078
| Epoch (UTC): | 08 September 2024 03:54:49 |
| Eccentricity: | 0.0001497 |
| inclination: | 41.4686° |
| perigee height: | 376 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 297.3488° |
| argument of perigee: | 52.7304° |
| revolutions per day: | 15.63544329 |
| mean anomaly at epoch: | 307.3672° |
| orbit number at epoch: | 19207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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