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 54821U 26145.18831981 +.00000000 +00000-0 +35102-4 0 00005
2 54821 43.0040 63.9694 0001311 265.4297 94.6405 15.27576948 03
| Epoch (UTC): | 25 May 2026 04:31:10 |
| Eccentricity: | 0.0001311 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 63.9694° |
| argument of perigee: | 265.4297° |
| revolutions per day: | 15.27576948 |
| mean anomaly at epoch: | 94.6405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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