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 52451U 26145.72202368 +.00000000 +00000-0 +47622-3 0 00002
2 52451 53.2010 53.5819 0009739 244.7053 115.2987 16.39390261 07
| Epoch (UTC): | 25 May 2026 17:19:42 |
| Eccentricity: | 0.0009739 |
| inclination: | 53.2010° |
| perigee height: | 161 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 53.5819° |
| argument of perigee: | 244.7053° |
| revolutions per day: | 16.39390261 |
| mean anomaly at epoch: | 115.2987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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