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 51970C 22025Q 24358.52548611 -.00003854 00000+0 -25822-3 0 3589
2 51970 53.0530 211.3643 0001454 88.5486 98.7111 15.06398711 12
| Epoch (UTC): | 23 December 2024 12:36:42 |
| Eccentricity: | 0.0001454 |
| inclination: | 53.0530° |
| perigee height: | 546 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 211.3643° |
| argument of perigee: | 88.5486° |
| revolutions per day: | 15.06398711 |
| mean anomaly at epoch: | 98.7111° |
| 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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