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 66781U 26145.61987705 +.00000000 +00000-0 +58592-3 0 00004
2 66781 97.5278 217.1355 0008059 192.2559 167.8470 14.99631702 02
| Epoch (UTC): | 25 May 2026 14:52:37 |
| Eccentricity: | 0.0008059 |
| inclination: | 97.5278° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 217.1355° |
| argument of perigee: | 192.2559° |
| revolutions per day: | 14.99631702 |
| mean anomaly at epoch: | 167.8470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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