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 54188U 26145.31628589 +.00000000 +00000-0 -47513-4 0 00004
2 54188 53.2111 10.2888 0000923 113.3216 246.7874 15.08838611 08
| Epoch (UTC): | 25 May 2026 07:35:27 |
| Eccentricity: | 0.0000923 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 10.2888° |
| argument of perigee: | 113.3216° |
| revolutions per day: | 15.08838611 |
| mean anomaly at epoch: | 246.7874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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