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 52479U 26145.48601179 +.00000000 +00000-0 +30980-4 0 00008
2 52479 53.2121 64.3677 0001175 96.8503 263.2622 15.08834334 03
| Epoch (UTC): | 25 May 2026 11:39:51 |
| Eccentricity: | 0.0001175 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.3677° |
| argument of perigee: | 96.8503° |
| revolutions per day: | 15.08834334 |
| mean anomaly at epoch: | 263.2622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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