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 54679U 26145.30812294 +.00000000 +00000-0 +13445-3 0 00001
2 54679 87.9249 248.5336 0002119 92.9158 267.2219 13.21818898 08
| Epoch (UTC): | 25 May 2026 07:23:41 |
| Eccentricity: | 0.0002119 |
| inclination: | 87.9249° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5336° |
| argument of perigee: | 92.9158° |
| revolutions per day: | 13.21818898 |
| mean anomaly at epoch: | 267.2219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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