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 66764U 26145.44892743 +.00000000 +00000-0 +11787-3 0 00008
2 66764 97.4205 219.3092 0004223 68.9369 291.2316 15.18757042 00
| Epoch (UTC): | 25 May 2026 10:46:27 |
| Eccentricity: | 0.0004223 |
| inclination: | 97.4205° |
| perigee height: | 507 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 219.3092° |
| argument of perigee: | 68.9369° |
| revolutions per day: | 15.18757042 |
| mean anomaly at epoch: | 291.2316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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