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 45140U 26145.62063713 +.00000000 +00000-0 -16215-2 0 00001
2 45140 87.8906 25.5649 0002353 76.6297 283.5093 13.10852579 06
| Epoch (UTC): | 25 May 2026 14:53:43 |
| Eccentricity: | 0.0002353 |
| inclination: | 87.8906° |
| perigee height: | 1218 km |
| apogee height: | 1222 km |
| right ascension of ascending node: | 25.5649° |
| argument of perigee: | 76.6297° |
| revolutions per day: | 13.10852579 |
| mean anomaly at epoch: | 283.5093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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