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 54205U 26145.33462588 +.00000000 +00000-0 -11756-3 0 00000
2 54205 53.2141 9.6933 0001491 94.0626 266.0537 15.08843756 02
| Epoch (UTC): | 25 May 2026 08:01:51 |
| Eccentricity: | 0.0001491 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 9.6933° |
| argument of perigee: | 94.0626° |
| revolutions per day: | 15.08843756 |
| mean anomaly at epoch: | 266.0537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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