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 52294U 26145.31948354 +.00000000 +00000-0 +35358-4 0 00008
2 52294 53.2134 115.1133 0001140 77.1197 282.9923 15.08845015 07
| Epoch (UTC): | 25 May 2026 07:40:03 |
| Eccentricity: | 0.0001140 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.1133° |
| argument of perigee: | 77.1197° |
| revolutions per day: | 15.08845015 |
| mean anomaly at epoch: | 282.9923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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