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 66251U 26145.12026169 +.00000000 +00000-0 +66258-3 0 00008
2 66251 53.1612 288.5054 0001325 90.3937 269.7216 15.31709341 01
| Epoch (UTC): | 25 May 2026 02:53:10 |
| Eccentricity: | 0.0001325 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 288.5054° |
| argument of perigee: | 90.3937° |
| revolutions per day: | 15.31709341 |
| mean anomaly at epoch: | 269.7216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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