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 53627U 26145.55911318 +.00000000 +00000-0 -20927-4 0 00002
2 53627 53.2151 248.7575 0001341 87.3514 272.7632 15.08839347 04
| Epoch (UTC): | 25 May 2026 13:25:07 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 248.7575° |
| argument of perigee: | 87.3514° |
| revolutions per day: | 15.08839347 |
| mean anomaly at epoch: | 272.7632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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