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 54054U 26145.00808087 +.00000000 +00000-0 +43275-4 0 00005
2 54054 53.2171 1.6415 0001523 96.1437 263.9729 15.08841052 09
| Epoch (UTC): | 25 May 2026 00:11:38 |
| Eccentricity: | 0.0001523 |
| inclination: | 53.2171° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 1.6415° |
| argument of perigee: | 96.1437° |
| revolutions per day: | 15.08841052 |
| mean anomaly at epoch: | 263.9729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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