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 25893U 99045B 24256.95823980 .00000341 00000-0 33172-3 0 9994
2 25893 82.9268 215.6083 0027060 258.8910 160.3730 13.76721682258522
| Epoch (UTC): | 12 September 2024 22:59:51 |
| Eccentricity: | 0.0027060 |
| inclination: | 82.9268° |
| perigee height: | 955 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 215.6083° |
| argument of perigee: | 258.8910° |
| revolutions per day: | 13.76721682 |
| mean anomaly at epoch: | 160.3730° |
| orbit number at epoch: | 25852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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