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 54104U 26145.47767243 +.00000000 +00000-0 +27359-4 0 00005
2 54104 53.2158 313.9590 0001273 93.7849 266.3289 15.08838394 08
| Epoch (UTC): | 25 May 2026 11:27:50 |
| Eccentricity: | 0.0001273 |
| inclination: | 53.2158° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 313.9590° |
| argument of perigee: | 93.7849° |
| revolutions per day: | 15.08838394 |
| mean anomaly at epoch: | 266.3289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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