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 25338U 26020.25129575 +.00000000 +00000-0 +10344-3 0 00005
2 25338 98.5195 44.7926 0011246 64.2549 295.9791 14.27088917 05
| Epoch (UTC): | 20 January 2026 06:01:51 |
| Eccentricity: | 0.0011246 |
| inclination: | 98.5195° |
| perigee height: | 793 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 44.7926° |
| argument of perigee: | 64.2549° |
| revolutions per day: | 14.27088917 |
| mean anomaly at epoch: | 295.9791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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