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 54000U 26145.48465049 +.00000000 +00000-0 -16760-4 0 00005
2 54000 53.2119 219.5631 0001252 85.1751 274.9384 15.08840917 06
| Epoch (UTC): | 25 May 2026 11:37:53 |
| Eccentricity: | 0.0001252 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 219.5631° |
| argument of perigee: | 85.1751° |
| revolutions per day: | 15.08840917 |
| mean anomaly at epoch: | 274.9384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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