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 66730U 26145.15540211 +.00000000 +00000-0 +28387-3 0 00003
2 66730 97.4172 219.1654 0002045 84.5070 275.6399 15.20159844 07
| Epoch (UTC): | 25 May 2026 03:43:46 |
| Eccentricity: | 0.0002045 |
| inclination: | 97.4172° |
| perigee height: | 504 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 219.1654° |
| argument of perigee: | 84.5070° |
| revolutions per day: | 15.20159844 |
| mean anomaly at epoch: | 275.6399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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