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 54673U 26145.55518528 +.00000000 +00000-0 +11540-3 0 00009
2 54673 87.9254 248.4844 0002547 92.0885 268.0541 13.21826729 03
| Epoch (UTC): | 25 May 2026 13:19:28 |
| Eccentricity: | 0.0002547 |
| inclination: | 87.9254° |
| perigee height: | 1176 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 248.4844° |
| argument of perigee: | 92.0885° |
| revolutions per day: | 13.21826729 |
| mean anomaly at epoch: | 268.0541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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