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 52379U 26145.44736477 +.00000000 +00000-0 -72520-4 0 00000
2 52379 53.2107 204.5431 0001243 79.6278 280.4855 15.08844085 09
| Epoch (UTC): | 25 May 2026 10:44:12 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.2107° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 204.5431° |
| argument of perigee: | 79.6278° |
| revolutions per day: | 15.08844085 |
| mean anomaly at epoch: | 280.4855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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