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 55146U 26145.30480521 +.00000000 +00000-0 +27922-5 0 00002
2 55146 87.9152 340.0443 0001549 100.2095 259.9212 13.18685711 00
| Epoch (UTC): | 25 May 2026 07:18:55 |
| Eccentricity: | 0.0001549 |
| inclination: | 87.9152° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0443° |
| argument of perigee: | 100.2095° |
| revolutions per day: | 13.18685711 |
| mean anomaly at epoch: | 259.9212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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