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 66280U 26145.38723462 +.00000000 +00000-0 +71551-3 0 00000
2 66280 53.1587 193.9690 0000863 96.3898 263.7203 15.34395094 06
| Epoch (UTC): | 25 May 2026 09:17:37 |
| Eccentricity: | 0.0000863 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 193.9690° |
| argument of perigee: | 96.3898° |
| revolutions per day: | 15.34395094 |
| mean anomaly at epoch: | 263.7203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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