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 51880U 26145.37560377 +.00000000 +00000-0 +12848-2 0 00006
2 51880 53.2128 24.5813 0001778 102.0992 258.0200 15.08750248 01
| Epoch (UTC): | 25 May 2026 09:00:52 |
| Eccentricity: | 0.0001778 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 24.5813° |
| argument of perigee: | 102.0992° |
| revolutions per day: | 15.08750248 |
| mean anomaly at epoch: | 258.0200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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