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 66784U 26145.13745817 +.00000000 +00000-0 +63412-3 0 00007
2 66784 97.5251 216.5703 0013185 207.4417 152.6112 14.98715184 05
| Epoch (UTC): | 25 May 2026 03:17:56 |
| Eccentricity: | 0.0013185 |
| inclination: | 97.5251° |
| perigee height: | 562 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 216.5703° |
| argument of perigee: | 207.4417° |
| revolutions per day: | 14.98715184 |
| mean anomaly at epoch: | 152.6112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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