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 26162.60960356 +.00000000 +00000-0 +29848-4 0 00001
2 25400 98.8362 116.7209 0010922 100.8867 259.3543 14.26067680 00
| Epoch (UTC): | 11 June 2026 14:37:49 |
| Eccentricity: | 0.0010922 |
| inclination: | 98.8362° |
| perigee height: | 797 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 116.7209° |
| argument of perigee: | 100.8867° |
| revolutions per day: | 14.26067680 |
| mean anomaly at epoch: | 259.3543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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