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 55814U 26145.41026170 +.00000000 +00000-0 +54294-3 0 00002
2 55814 87.8935 294.2541 0001934 100.3213 259.8135 13.14503466 05
| Epoch (UTC): | 25 May 2026 09:50:46 |
| Eccentricity: | 0.0001934 |
| inclination: | 87.8935° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2541° |
| argument of perigee: | 100.3213° |
| revolutions per day: | 13.14503466 |
| mean anomaly at epoch: | 259.8135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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