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 25280U 98020A 25199.35586485 .17841747 26209-5 25274-3 0 9992
2 25280 97.3829 53.7423 0011362 249.3529 283.8722 16.48395503499411
| Epoch (UTC): | 18 July 2025 08:32:26 |
| Eccentricity: | 0.0011362 |
| inclination: | 97.3829° |
| perigee height: | 136 km |
| apogee height: | 151 km |
| right ascension of ascending node: | 53.7423° |
| argument of perigee: | 249.3529° |
| revolutions per day: | 16.48395503 |
| mean anomaly at epoch: | 283.8722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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