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 66897U 26145.58335647 +.00000000 +00000-0 +23298-1 0 00003
2 66897 53.1597 27.1100 0002015 155.6218 268.0821 15.33628428 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002015 |
| inclination: | 53.1597° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 27.1100° |
| argument of perigee: | 155.6218° |
| revolutions per day: | 15.33628428 |
| mean anomaly at epoch: | 268.0821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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