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 52847U 26145.02186471 +.00000000 +00000-0 +36537-4 0 00004
2 52847 53.2147 51.4502 0001322 90.5974 269.5170 15.08839514 03
| Epoch (UTC): | 25 May 2026 00:31:29 |
| Eccentricity: | 0.0001322 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 51.4502° |
| argument of perigee: | 90.5974° |
| revolutions per day: | 15.08839514 |
| mean anomaly at epoch: | 269.5170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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