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 68544U 26145.33862583 +.00000000 +00000-0 +54281-3 0 00009
2 68544 53.1603 6.3053 0000905 115.1851 244.9245 15.34398458 00
| Epoch (UTC): | 25 May 2026 08:07:37 |
| Eccentricity: | 0.0000905 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 6.3053° |
| argument of perigee: | 115.1851° |
| revolutions per day: | 15.34398458 |
| mean anomaly at epoch: | 244.9245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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