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 51897U 26145.36916463 +.00000000 +00000-0 +29282-4 0 00006
2 51897 53.2138 14.8915 0001142 101.4702 258.6419 15.08842119 09
| Epoch (UTC): | 25 May 2026 08:51:35 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 14.8915° |
| argument of perigee: | 101.4702° |
| revolutions per day: | 15.08842119 |
| mean anomaly at epoch: | 258.6419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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