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 25520U 26154.07323266 +.00000000 +00000-0 +30242-3 0 00008
2 25520 28.4319 44.4539 0001007 5.9725 354.0897 15.89560050 03
| Epoch (UTC): | 03 June 2026 01:45:27 |
| Eccentricity: | 0.0001007 |
| inclination: | 28.4319° |
| perigee height: | 303 km |
| apogee height: | 304 km |
| right ascension of ascending node: | 44.4539° |
| argument of perigee: | 5.9725° |
| revolutions per day: | 15.89560050 |
| mean anomaly at epoch: | 354.0897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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