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 26129.49280046 +.00000000 +00000-0 +31430-4 0 00002
2 25400 98.8340 83.3251 0009506 192.2391 167.8558 14.26062309 07
| Epoch (UTC): | 09 May 2026 11:49:37 |
| Eccentricity: | 0.0009506 |
| inclination: | 98.8340° |
| perigee height: | 798 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 83.3251° |
| argument of perigee: | 192.2391° |
| revolutions per day: | 14.26062309 |
| mean anomaly at epoch: | 167.8558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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