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 25756U 26104.08495066 +.00000000 +00000-0 +42125-4 0 00007
2 25756 98.6243 137.5785 0014442 98.4414 261.8420 14.55769414 09
| Epoch (UTC): | 14 April 2026 02:02:19 |
| Eccentricity: | 0.0014442 |
| inclination: | 98.6243° |
| perigee height: | 697 km |
| apogee height: | 717 km |
| right ascension of ascending node: | 137.5785° |
| argument of perigee: | 98.4414° |
| revolutions per day: | 14.55769414 |
| mean anomaly at epoch: | 261.8420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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