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 52553U 26145.66668980 +.00000000 +00000-0 +14038-1 0 00007
2 52553 53.2198 137.0925 0001339 85.8860 140.9963 15.58713164 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001339 |
| inclination: | 53.2198° |
| perigee height: | 390 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 137.0925° |
| argument of perigee: | 85.8860° |
| revolutions per day: | 15.58713164 |
| mean anomaly at epoch: | 140.9963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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