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 54087U 26145.55726906 +.00000000 +00000-0 +81706-5 0 00002
2 54087 53.2132 348.6886 0001309 88.6174 271.4968 15.08834562 01
| Epoch (UTC): | 25 May 2026 13:22:28 |
| Eccentricity: | 0.0001309 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.6886° |
| argument of perigee: | 88.6174° |
| revolutions per day: | 15.08834562 |
| mean anomaly at epoch: | 271.4968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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