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 66829U 26145.37155547 +.00000000 +00000-0 +34226-3 0 00009
2 66829 70.0003 141.0524 0004304 264.4379 95.6289 14.98340998 00
| Epoch (UTC): | 25 May 2026 08:55:02 |
| Eccentricity: | 0.0004304 |
| inclination: | 70.0003° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.0524° |
| argument of perigee: | 264.4379° |
| revolutions per day: | 14.98340998 |
| mean anomaly at epoch: | 95.6289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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