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 48881C 21059C 24358.52826389 .00018361 00000+0 14342-2 0 3584
2 48881 97.6591 120.1304 0002713 251.2871 206.3653 15.01190343 11
| Epoch (UTC): | 23 December 2024 12:40:42 |
| Eccentricity: | 0.0002713 |
| inclination: | 97.6591° |
| perigee height: | 561 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 120.1304° |
| argument of perigee: | 251.2871° |
| revolutions per day: | 15.01190343 |
| mean anomaly at epoch: | 206.3653° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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