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 66753U 26145.13992515 +.00000000 +00000-0 +21762-3 0 00004
2 66753 97.4177 218.5091 0005097 110.8154 249.3622 15.10231534 04
| Epoch (UTC): | 25 May 2026 03:21:29 |
| Eccentricity: | 0.0005097 |
| inclination: | 97.4177° |
| perigee height: | 532 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 218.5091° |
| argument of perigee: | 110.8154° |
| revolutions per day: | 15.10231534 |
| mean anomaly at epoch: | 249.3622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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