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 54253U 26145.58858358 +.00000000 +00000-0 +48447-3 0 00000
2 54253 97.6185 284.6931 0006418 93.8484 266.3501 15.51233447 03
| Epoch (UTC): | 25 May 2026 14:07:33 |
| Eccentricity: | 0.0006418 |
| inclination: | 97.6185° |
| perigee height: | 409 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 284.6931° |
| argument of perigee: | 93.8484° |
| revolutions per day: | 15.51233447 |
| mean anomaly at epoch: | 266.3501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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