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 66245U 26145.11551093 +.00000000 +00000-0 +41748-3 0 00006
2 66245 53.1606 289.1841 0001092 101.5978 258.5145 15.30206459 07
| Epoch (UTC): | 25 May 2026 02:46:20 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 289.1841° |
| argument of perigee: | 101.5978° |
| revolutions per day: | 15.30206459 |
| mean anomaly at epoch: | 258.5145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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