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 25479U 26065.80659883 +.00000000 +00000-0 +48703-3 0 00001
2 25479 45.0062 101.4505 0002969 152.5206 207.5800 14.38878120 03
| Epoch (UTC): | 06 March 2026 19:21:30 |
| Eccentricity: | 0.0002969 |
| inclination: | 45.0062° |
| perigee height: | 760 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 101.4505° |
| argument of perigee: | 152.5206° |
| revolutions per day: | 14.38878120 |
| mean anomaly at epoch: | 207.5800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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