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 26156.36378609 +.00000000 +00000-0 +22963-3 0 00000
2 25733 98.6815 200.0845 0013892 208.4266 151.6153 14.18931900 07
| Epoch (UTC): | 05 June 2026 08:43:51 |
| Eccentricity: | 0.0013892 |
| inclination: | 98.6815° |
| perigee height: | 819 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 200.0845° |
| argument of perigee: | 208.4266° |
| revolutions per day: | 14.18931900 |
| mean anomaly at epoch: | 151.6153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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