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 25991U 99067A 24340.58369500 .00000445 00000-0 24327-3 0 9990
2 25991 99.0563 359.2840 0010426 145.9542 326.2188 14.17227735291511
| Epoch (UTC): | 05 December 2024 14:00:31 |
| Eccentricity: | 0.0010426 |
| inclination: | 99.0563° |
| perigee height: | 827 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 359.2840° |
| argument of perigee: | 145.9542° |
| revolutions per day: | 14.17227735 |
| mean anomaly at epoch: | 326.2188° |
| orbit number at epoch: | 29151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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