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 52478U 26145.53659606 +.00000000 +00000-0 +15836-3 0 00003
2 52478 53.2169 74.1394 0001173 79.0451 281.0673 15.08852334 06
| Epoch (UTC): | 25 May 2026 12:52:41 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.2169° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.1394° |
| argument of perigee: | 79.0451° |
| revolutions per day: | 15.08852334 |
| mean anomaly at epoch: | 281.0673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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