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 26087.99371378 +.00000000 +00000-0 +36452-3 0 00007
2 25725 28.3183 322.0892 2385214 121.1415 264.4809 9.67478917 05
| Epoch (UTC): | 28 March 2026 23:50:56 |
| Eccentricity: | 0.2385214 |
| inclination: | 28.3183° |
| perigee height: | 706 km |
| apogee height: | 5144 km |
| right ascension of ascending node: | 322.0892° |
| argument of perigee: | 121.1415° |
| revolutions per day: | 9.67478917 |
| mean anomaly at epoch: | 264.4809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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