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 25399U 98043F 25073.46729163 .00000390 00000-0 18501-3 0 9997
2 25399 98.9248 46.0185 0002146 31.8166 328.3142 14.25418487385836
| Epoch (UTC): | 14 March 2025 11:12:53 |
| Eccentricity: | 0.0002146 |
| inclination: | 98.9248° |
| perigee height: | 805 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 46.0185° |
| argument of perigee: | 31.8166° |
| revolutions per day: | 14.25418487 |
| mean anomaly at epoch: | 328.3142° |
| orbit number at epoch: | 38583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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