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 25397U 98043D 24338.20835891 .00000354 00000-0 17356-3 0 9993
2 25397 98.9468 307.6675 0002095 56.2024 303.9353 14.24203460371699
| Epoch (UTC): | 03 December 2024 05:00:02 |
| Eccentricity: | 0.0002095 |
| inclination: | 98.9468° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 307.6675° |
| argument of perigee: | 56.2024° |
| revolutions per day: | 14.24203460 |
| mean anomaly at epoch: | 303.9353° |
| orbit number at epoch: | 37169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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