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 48066U 26145.21915437 +.00000000 +00000-0 -77776-3 0 00005
2 48066 87.8940 324.7950 0001670 89.8824 270.2496 13.13468418 04
| Epoch (UTC): | 25 May 2026 05:15:34 |
| Eccentricity: | 0.0001670 |
| inclination: | 87.8940° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7950° |
| argument of perigee: | 89.8824° |
| revolutions per day: | 13.13468418 |
| mean anomaly at epoch: | 270.2496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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