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 52864U 26145.11110544 +.00000000 +00000-0 -40690-5 0 00008
2 52864 53.2158 41.0507 0001361 95.4996 264.6152 15.08843083 07
| Epoch (UTC): | 25 May 2026 02:39:59 |
| Eccentricity: | 0.0001361 |
| inclination: | 53.2158° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 41.0507° |
| argument of perigee: | 95.4996° |
| revolutions per day: | 15.08843083 |
| mean anomaly at epoch: | 264.6152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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