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 25397U 26017.88306750 +.00000000 +00000-0 +47790-4 0 00003
2 25397 98.9956 6.9365 0000498 337.8220 22.2936 14.24388662 07
| Epoch (UTC): | 17 January 2026 21:11:37 |
| Eccentricity: | 0.0000498 |
| inclination: | 98.9956° |
| perigee height: | 810 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 6.9365° |
| argument of perigee: | 337.8220° |
| revolutions per day: | 14.24388662 |
| mean anomaly at epoch: | 22.2936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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