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 66887U 26145.58335647 +.00000000 +00000-0 +17328-2 0 00000
2 66887 53.1594 27.0211 0001310 102.9712 6.4072 15.34350788 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001310 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 27.0211° |
| argument of perigee: | 102.9712° |
| revolutions per day: | 15.34350788 |
| mean anomaly at epoch: | 6.4072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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