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 65572U 26145.38506696 +.00000000 +00000-0 +64693-4 0 00001
2 65572 81.3069 31.9057 0005892 253.8594 106.1914 13.84281886 00
| Epoch (UTC): | 25 May 2026 09:14:29 |
| Eccentricity: | 0.0005892 |
| inclination: | 81.3069° |
| perigee height: | 944 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 31.9057° |
| argument of perigee: | 253.8594° |
| revolutions per day: | 13.84281886 |
| mean anomaly at epoch: | 106.1914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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