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 25733U 26162.56912620 +.00000000 +00000-0 +19237-3 0 00006
2 25733 98.6811 206.1632 0014281 190.2952 169.7934 14.18937320 06
| Epoch (UTC): | 11 June 2026 13:39:32 |
| Eccentricity: | 0.0014281 |
| inclination: | 98.6811° |
| perigee height: | 819 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 206.1632° |
| argument of perigee: | 190.2952° |
| revolutions per day: | 14.18937320 |
| mean anomaly at epoch: | 169.7934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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