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 52491U 26145.47497455 +.00000000 +00000-0 +85678-4 0 00005
2 52491 53.2128 64.4175 0001539 90.4778 269.6391 15.08831172 06
| Epoch (UTC): | 25 May 2026 11:23:57 |
| Eccentricity: | 0.0001539 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.4175° |
| argument of perigee: | 90.4778° |
| revolutions per day: | 15.08831172 |
| mean anomaly at epoch: | 269.6391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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