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 54789U 26145.41008176 +.00000000 +00000-0 -72651-4 0 00007
2 54789 53.2149 29.4751 0001339 106.3734 253.7405 15.08836706 07
| Epoch (UTC): | 25 May 2026 09:50:31 |
| Eccentricity: | 0.0001339 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.4751° |
| argument of perigee: | 106.3734° |
| revolutions per day: | 15.08836706 |
| mean anomaly at epoch: | 253.7405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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