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 25725U 26040.38762120 +.00000000 +00000-0 +36294-3 0 00002
2 25725 28.3332 87.5436 2383860 276.3785 57.2953 9.67464732 04
| Epoch (UTC): | 09 February 2026 09:18:10 |
| Eccentricity: | 0.2383860 |
| inclination: | 28.3332° |
| perigee height: | 708 km |
| apogee height: | 5143 km |
| right ascension of ascending node: | 87.5436° |
| argument of perigee: | 276.3785° |
| revolutions per day: | 9.67464732 |
| mean anomaly at epoch: | 57.2953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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