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 26145.44610883 +.00000000 +00000-0 +43712-4 0 00002
2 25397 99.0063 137.6323 0000349 329.3516 30.7641 14.24423288 04
| Epoch (UTC): | 25 May 2026 10:42:23 |
| Eccentricity: | 0.0000349 |
| inclination: | 99.0063° |
| perigee height: | 810 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 137.6323° |
| argument of perigee: | 329.3516° |
| revolutions per day: | 14.24423288 |
| mean anomaly at epoch: | 30.7641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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