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 54125U 26145.37533269 +.00000000 +00000-0 +14984-3 0 00005
2 54125 87.9150 309.5239 0001655 89.0532 271.0791 13.19726204 06
| Epoch (UTC): | 25 May 2026 09:00:28 |
| Eccentricity: | 0.0001655 |
| inclination: | 87.9150° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5239° |
| argument of perigee: | 89.0532° |
| revolutions per day: | 13.19726204 |
| mean anomaly at epoch: | 271.0791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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