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 66756U 26145.61892277 +.00000000 +00000-0 +32691-3 0 00007
2 66756 97.4212 219.7075 0002833 67.2906 292.8628 15.20302395 01
| Epoch (UTC): | 25 May 2026 14:51:14 |
| Eccentricity: | 0.0002833 |
| inclination: | 97.4212° |
| perigee height: | 503 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 219.7075° |
| argument of perigee: | 67.2906° |
| revolutions per day: | 15.20302395 |
| mean anomaly at epoch: | 292.8628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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