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 48865U 26145.65713551 +.00000000 +00000-0 +14346-3 0 00006
2 48865 67.1415 168.0534 0008173 272.2958 87.7260 15.33713497 01
| Epoch (UTC): | 25 May 2026 15:46:16 |
| Eccentricity: | 0.0008173 |
| inclination: | 67.1415° |
| perigee height: | 459 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 168.0534° |
| argument of perigee: | 272.2958° |
| revolutions per day: | 15.33713497 |
| mean anomaly at epoch: | 87.7260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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