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 66653U 26145.35212755 +.00000000 +00000-0 +16976-3 0 00009
2 66653 97.7483 74.7995 0014192 73.4118 286.8658 14.92679606 01
| Epoch (UTC): | 25 May 2026 08:27:03 |
| Eccentricity: | 0.0014192 |
| inclination: | 97.7483° |
| perigee height: | 580 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 74.7995° |
| argument of perigee: | 73.4118° |
| revolutions per day: | 14.92679606 |
| mean anomaly at epoch: | 286.8658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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