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 48067U 26145.45615491 +.00000000 +00000-0 -52526-3 0 00005
2 48067 87.8939 324.7495 0001648 76.6998 283.4315 13.13468947 01
| Epoch (UTC): | 25 May 2026 10:56:51 |
| Eccentricity: | 0.0001648 |
| inclination: | 87.8939° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7495° |
| argument of perigee: | 76.6998° |
| revolutions per day: | 13.13468947 |
| mean anomaly at epoch: | 283.4315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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