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 54845U 26145.13370794 +.00000000 +00000-0 +14659-4 0 00000
2 54845 43.0023 61.0089 0000513 267.0152 93.0641 15.27587255 06
| Epoch (UTC): | 25 May 2026 03:12:32 |
| Eccentricity: | 0.0000513 |
| inclination: | 43.0023° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 61.0089° |
| argument of perigee: | 267.0152° |
| revolutions per day: | 15.27587255 |
| mean anomaly at epoch: | 93.0641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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