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 24298U 96051B 25312.70641448 -.00000033 00000-0 89909-5 0 9990
2 24298 70.7598 71.3173 0017866 304.5038 55.4394 14.12392409504561
| Epoch (UTC): | 08 November 2025 16:57:14 |
| Eccentricity: | 0.0017866 |
| inclination: | 70.7598° |
| perigee height: | 838 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 71.3173° |
| argument of perigee: | 304.5038° |
| revolutions per day: | 14.12392409 |
| mean anomaly at epoch: | 55.4394° |
| orbit number at epoch: | 50456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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