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 66779U 26145.12812497 +.00000000 +00000-0 +22088-3 0 00003
2 66779 97.4188 218.7726 0004763 201.4341 158.6694 15.18260365 08
| Epoch (UTC): | 25 May 2026 03:04:29 |
| Eccentricity: | 0.0004763 |
| inclination: | 97.4188° |
| perigee height: | 508 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 218.7726° |
| argument of perigee: | 201.4341° |
| revolutions per day: | 15.18260365 |
| mean anomaly at epoch: | 158.6694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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