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 52999U 26145.31442799 +.00000000 +00000-0 +12397-3 0 00009
2 52999 53.2144 110.1370 0001269 75.6695 284.4438 15.08844906 02
| Epoch (UTC): | 25 May 2026 07:32:46 |
| Eccentricity: | 0.0001269 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.1370° |
| argument of perigee: | 75.6695° |
| revolutions per day: | 15.08844906 |
| mean anomaly at epoch: | 284.4438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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