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 66467U 26145.53386771 +.00000000 +00000-0 +68743-3 0 00001
2 66467 43.0025 222.6381 0001852 262.5756 97.4885 15.27588462 07
| Epoch (UTC): | 25 May 2026 12:48:46 |
| Eccentricity: | 0.0001852 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.6381° |
| argument of perigee: | 262.5756° |
| revolutions per day: | 15.27588462 |
| mean anomaly at epoch: | 97.4885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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