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 54095U 26145.56095042 +.00000000 +00000-0 +27588-4 0 00009
2 54095 53.2130 348.7041 0001183 83.1105 277.0022 15.08837118 09
| Epoch (UTC): | 25 May 2026 13:27:46 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.7041° |
| argument of perigee: | 83.1105° |
| revolutions per day: | 15.08837118 |
| mean anomaly at epoch: | 277.0022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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