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 is defined by the following mean orbital elements,
1 25400U 26018.35404542 +.00000000 +00000-0 +35123-4 0 00006
2 25400 98.8175 331.3866 0010211 154.8652 205.3027 14.26035118 07
| Epoch (UTC): | 18 January 2026 08:29:49 |
| Eccentricity: | 0.0010211 |
| inclination: | 98.8175° |
| perigee height: | 798 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 331.3866° |
| argument of perigee: | 154.8652° |
| revolutions per day: | 14.26035118 |
| mean anomaly at epoch: | 205.3027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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