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 51885U 26145.33605816 +.00000000 +00000-0 +23824-3 0 00002
2 51885 53.2129 15.0424 0001323 94.6095 265.5049 15.08819352 02
| Epoch (UTC): | 25 May 2026 08:03:55 |
| Eccentricity: | 0.0001323 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 15.0424° |
| argument of perigee: | 94.6095° |
| revolutions per day: | 15.08819352 |
| mean anomaly at epoch: | 265.5049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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