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 52469U 26145.49613483 +.00000000 +00000-0 +20295-4 0 00007
2 52469 53.2118 74.3292 0001293 82.0895 278.0244 15.08828374 05
| Epoch (UTC): | 25 May 2026 11:54:26 |
| Eccentricity: | 0.0001293 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.3292° |
| argument of perigee: | 82.0895° |
| revolutions per day: | 15.08828374 |
| mean anomaly at epoch: | 278.0244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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