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 48079U 26145.64903866 +.00000000 +00000-0 +49215-4 0 00006
2 48079 97.9921 143.9229 0003775 322.4708 37.6239 14.80274996 05
| Epoch (UTC): | 25 May 2026 15:34:36 |
| Eccentricity: | 0.0003775 |
| inclination: | 97.9921° |
| perigee height: | 626 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 143.9229° |
| argument of perigee: | 322.4708° |
| revolutions per day: | 14.80274996 |
| mean anomaly at epoch: | 37.6239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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