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 25399U 26162.93992873 +.00000000 +00000-0 +50771-4 0 00002
2 25399 98.9762 149.8838 0002729 113.5954 246.5512 14.25618755 09
| Epoch (UTC): | 11 June 2026 22:33:29 |
| Eccentricity: | 0.0002729 |
| inclination: | 98.9762° |
| perigee height: | 804 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 149.8838° |
| argument of perigee: | 113.5954° |
| revolutions per day: | 14.25618755 |
| mean anomaly at epoch: | 246.5512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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