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 52631U 26145.34896862 +.00000000 +00000-0 +70232-5 0 00003
2 52631 53.2151 284.9901 0001255 98.2345 261.8789 15.08834727 09
| Epoch (UTC): | 25 May 2026 08:22:30 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.9901° |
| argument of perigee: | 98.2345° |
| revolutions per day: | 15.08834727 |
| mean anomaly at epoch: | 261.8789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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