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 52676U 26145.34570521 +.00000000 +00000-0 +27104-4 0 00002
2 52676 53.2143 169.9977 0001245 82.5405 277.5728 15.08843440 05
| Epoch (UTC): | 25 May 2026 08:17:48 |
| Eccentricity: | 0.0001245 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 169.9977° |
| argument of perigee: | 82.5405° |
| revolutions per day: | 15.08843440 |
| mean anomaly at epoch: | 277.5728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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