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 54796U 26145.13453646 +.00000000 +00000-0 +29788-5 0 00003
2 54796 53.2141 45.6924 0001377 71.5925 288.5217 15.08838472 05
| Epoch (UTC): | 25 May 2026 03:13:43 |
| Eccentricity: | 0.0001377 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 45.6924° |
| argument of perigee: | 71.5925° |
| revolutions per day: | 15.08838472 |
| mean anomaly at epoch: | 288.5217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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