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 66874U 26145.04969556 +.00000000 +00000-0 +57512-3 0 00009
2 66874 42.9978 272.2414 0000988 292.4610 67.6137 15.27587108 07
| Epoch (UTC): | 25 May 2026 01:11:33 |
| Eccentricity: | 0.0000988 |
| inclination: | 42.9978° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.2414° |
| argument of perigee: | 292.4610° |
| revolutions per day: | 15.27587108 |
| mean anomaly at epoch: | 67.6137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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