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 52455U 26145.20913028 +.00000000 +00000-0 -13855-5 0 00005
2 52455 53.2152 85.6118 0001537 87.9836 272.1333 15.08841915 00
| Epoch (UTC): | 25 May 2026 05:01:08 |
| Eccentricity: | 0.0001537 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 85.6118° |
| argument of perigee: | 87.9836° |
| revolutions per day: | 15.08841915 |
| mean anomaly at epoch: | 272.1333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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