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 53551U 26145.51959694 +.00000000 +00000-0 +80760-4 0 00003
2 53551 53.2133 79.2163 0001407 87.3171 272.7982 15.08828399 05
| Epoch (UTC): | 25 May 2026 12:28:13 |
| Eccentricity: | 0.0001407 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 79.2163° |
| argument of perigee: | 87.3171° |
| revolutions per day: | 15.08828399 |
| mean anomaly at epoch: | 272.7982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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