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 54012U 26145.38892968 +.00000000 +00000-0 +75258-4 0 00007
2 54012 53.2148 219.6804 0001188 86.1994 273.9134 15.08841339 03
| Epoch (UTC): | 25 May 2026 09:20:03 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 219.6804° |
| argument of perigee: | 86.1994° |
| revolutions per day: | 15.08841339 |
| mean anomaly at epoch: | 273.9134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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