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 66719U 26145.17777846 +.00000000 +00000-0 +28476-3 0 00007
2 66719 97.4240 219.1403 0006028 89.2531 270.9394 15.19490180 03
| Epoch (UTC): | 25 May 2026 04:16:00 |
| Eccentricity: | 0.0006028 |
| inclination: | 97.4240° |
| perigee height: | 503 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 219.1403° |
| argument of perigee: | 89.2531° |
| revolutions per day: | 15.19490180 |
| mean anomaly at epoch: | 270.9394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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