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 54588U 26145.60263051 +.00000000 +00000-0 +87138-4 0 00005
2 54588 98.2426 165.4043 0010715 42.7942 317.4083 14.46054590 02
| Epoch (UTC): | 25 May 2026 14:27:47 |
| Eccentricity: | 0.0010715 |
| inclination: | 98.2426° |
| perigee height: | 731 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 165.4043° |
| argument of perigee: | 42.7942° |
| revolutions per day: | 14.46054590 |
| mean anomaly at epoch: | 317.4083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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