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 66778U 26145.46127061 +.00000000 +00000-0 +22363-3 0 00001
2 66778 97.4206 219.1515 0002951 152.0747 208.0646 15.18457545 02
| Epoch (UTC): | 25 May 2026 11:04:13 |
| Eccentricity: | 0.0002951 |
| inclination: | 97.4206° |
| perigee height: | 508 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 219.1515° |
| argument of perigee: | 152.0747° |
| revolutions per day: | 15.18457545 |
| mean anomaly at epoch: | 208.0646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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