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 48618U 26145.48864395 +.00000000 +00000-0 +00000-0 0 00005
2 48618 5.1321 328.9697 0001529 92.9071 90.9106 1.00271666 04
| Epoch (UTC): | 25 May 2026 11:43:38 |
| Eccentricity: | 0.0001529 |
| inclination: | 5.1321° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 328.9697° |
| argument of perigee: | 92.9071° |
| revolutions per day: | 1.00271666 |
| mean anomaly at epoch: | 90.9106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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