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 48365U 26145.26637094 +.00000000 +00000-0 +82218-4 0 00009
2 48365 53.1589 351.6963 0001557 79.8995 280.2182 15.31709056 07
| Epoch (UTC): | 25 May 2026 06:23:34 |
| Eccentricity: | 0.0001557 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 351.6963° |
| argument of perigee: | 79.8995° |
| revolutions per day: | 15.31709056 |
| mean anomaly at epoch: | 280.2182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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